add axisymmetric jet case, SA

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)