From 2b42bfd7f7828e309bd711e5ab765f4e1ad1af9d Mon Sep 17 00:00:00 2001 From: bigfooted Date: Wed, 7 Aug 2024 10:54:10 +0200 Subject: [PATCH] add axisymmetric jet case, SA --- TestCases/vandv/inc_rans/jet/jet_sa.cfg | 167 ++++++++++++++++++++++++ 1 file changed, 167 insertions(+) create mode 100644 TestCases/vandv/inc_rans/jet/jet_sa.cfg diff --git a/TestCases/vandv/inc_rans/jet/jet_sa.cfg b/TestCases/vandv/inc_rans/jet/jet_sa.cfg new file mode 100644 index 00000000000..1a8b8f83095 --- /dev/null +++ b/TestCases/vandv/inc_rans/jet/jet_sa.cfg @@ -0,0 +1,167 @@ +%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% +% % +% SU2 configuration file % +% Case description: Turbulent axisymmetric jet % +% Author: Nijso Beishuizen % +% Institution: SU2 Foundation % +% Date: 2024.01.01 % +% File Version 8.0.1 "Harrier" % +% % +%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% + +% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------% +% +SOLVER= INC_RANS +% +KIND_TURB_MODEL= SA +SA_OPTIONS= NONE +% +RESTART_SOL= YES + +% +% --------------------------- VISCOSITY MODEL ---------------------------------% +VISCOSITY_MODEL= CONSTANT_VISCOSITY +MU_CONSTANT= 0.001 + +CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY +THERMAL_CONDUCTIVITY_CONSTANT= 0.6 +TURBULENT_CONDUCTIVITY_MODEL= NONE + +% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------% +INC_NONDIM= DIMENSIONAL +INC_DENSITY_MODEL= CONSTANT +INC_DENSITY_INIT= 1000.0 + +FLUID_MODEL= CONSTANT_DENSITY +SPECIFIC_HEAT_CP= 1000.0 +INC_TEMPERATURE_INIT= 300.00 +INC_ENERGY_EQUATION= NO +INC_VELOCITY_INIT= (0.5, 0.0, 0.0 ) +INC_INLET_TYPE= VELOCITY_INLET, VELOCITY_INLET +INC_OUTLET_TYPE= PRESSURE_OUTLET + +FREESTREAM_DENSITY= 1000.0 +FREESTREAM_VISCOSITY= 0.001 +FREESTREAM_VELOCITY= (0.5, 0.0, 0.0) +% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------% +% +% +% Free-stream temperature (288.15 K by default) +FREESTREAM_TEMPERATURE= 300.0 +% +% Reynolds number (non-dimensional, based on the free-stream values) +REYNOLDS_NUMBER= 2000.0 +% +% Reynolds length (in meters) +REYNOLDS_LENGTH= 0.001 + +% ---------------------- REFERENCE VALUE DEFINITION ---------------------------% +% +% Reference origin for moment computation +REF_ORIGIN_MOMENT_X = 0.25 +REF_ORIGIN_MOMENT_Y = 0.00 +REF_ORIGIN_MOMENT_Z = 0.00 +% +% Reference length for pitching, rolling, and yawing non-dimensional moment +REF_LENGTH= 0.001 +% +% Reference area for force coefficients (0 implies automatic calculation) +REF_AREA= 0.001 + +% -------------------- BOUNDARY CONDITION DEFINITION --------------------------% +% +AXISYMMETRIC= YES +% +MARKER_INLET= ( inlet_jet, 300.0, 56.2, 1.0, 0.0, 0.0,inlet_coflow,300.0,0.5,1.0,0.0,0.0 ) +% +MARKER_OUTLET= ( outlet, 0.0) +MARKER_HEATFLUX=(wall_edge,0.0, wall, 0.0, freestream, 0.0) +MARKER_FAR= (freestream) +% +MARKER_SYM= ( symmetry ) +% +MARKER_INLET_TURBULENT= ( inlet_jet, 0.02,10, inlet_coflow, 0.02,10) +% Control lower limit constants of the SST model (C*phi_infinity) +LOWER_LIMIT_K_FACTOR= 1e-20 +LOWER_LIMIT_OMEGA_FACTOR= 1e-6 + +% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------% +% +NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES +CFL_NUMBER=100 +CFL_ADAPT= NO +CFL_ADAPT_PARAM= ( 0.95, 1.01, 1.0, 200.0, 0.001 ) +ITER= 99999 +INC_INLET_DAMPING=0.01 +INC_OUTLET_DAMPING= 0.01 +% ----------------------- SLOPE LIMITER DEFINITION ----------------------------% +% +VENKAT_LIMITER_COEFF= 0.1 +ADJ_SHARP_LIMITER_COEFF= 3.0 +REF_SHARP_EDGES= 3.0 +SENS_REMOVE_SHARP= NO + +% -------------------------- MULTIGRID PARAMETERS -----------------------------% +% +MGLEVEL= 0 +% +% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------% +% +CONV_NUM_METHOD_FLOW= FDS +MUSCL_FLOW= NO +SLOPE_LIMITER_FLOW= NONE +JST_SENSOR_COEFF= ( 0.5, 0.02 ) +TIME_DISCRE_FLOW= EULER_IMPLICIT + +% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------% +% +CONV_NUM_METHOD_TURB= SCALAR_UPWIND +MUSCL_TURB= NO +SLOPE_LIMITER_TURB= VENKATAKRISHNAN +TIME_DISCRE_TURB= EULER_IMPLICIT +% ------------------------ LINEAR SOLVER DEFINITION ---------------------------% +% +LINEAR_SOLVER= FGMRES +LINEAR_SOLVER_PREC= ILU +LINEAR_SOLVER_ERROR= 1E-6 +LINEAR_SOLVER_ITER= 5 + +% --------------------------- CONVERGENCE PARAMETERS --------------------------% +% +CONV_RESIDUAL_MINVAL= -15 +CONV_STARTITER= 10 +CONV_CAUCHY_ELEMS= 100 +CONV_CAUCHY_EPS= 1E-6 +% + +% ------------------------- INPUT/OUTPUT INFORMATION --------------------------% +% +MESH_FILENAME= jet_inlet_medium.su2 +% +MESH_FORMAT= SU2 +% +MESH_OUT_FILENAME= mesh_out.su2 +% +SOLUTION_FILENAME= solution_flow_sa.dat +% +SOLUTION_ADJ_FILENAME= solution_adj.dat +% +TABULAR_FORMAT= CSV +% +CONV_FILENAME= history +% +RESTART_FILENAME= restart_flow_sa.dat +% +VOLUME_FILENAME= flow +% +% +% Output file surface flow coefficient (w/o extension) +SURFACE_FILENAME= surface_flow +% +% Writing solution file frequency +OUTPUT_WRT_FREQ= 100 +% +% +SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_PRESSURE, RMS_MOMENTUM-X, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_TKE, RMS_DISSIPATION, LINSOL_ITER, LINSOL_RESIDUAL, AVG_CFL) +OUTPUT_FILES= RESTART, PARAVIEW_MULTIBLOCK +VOLUME_OUTPUT= (PRIMITIVE,SOLUTION,RESIDUAL)