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Cristopher-MoralesCristopher-Morales
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adding test case using CONSTANT_CONDUCTIVITY model
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‎TestCases/parallel_regression.py‎

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turb_flatplate_species.test_vals = [-4.243064, -0.634797, -1.706652, 1.231264, -3.266203, 9.000000, -6.632972, 5.000000, -6.985977, 10.000000, -6.007208, 0.996237, 0.996237]
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test_list.append(turb_flatplate_species)
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# Flat plate (compressible) species transport using constant conductivity model
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turb_flatplate_species = TestCase('turb_flatplate_species_ConstConductivity')
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turb_flatplate_species.cfg_dir = "rans/flatplate"
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turb_flatplate_species.cfg_file = "turb_SA_flatplate_species_ConstConductivity.cfg"
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turb_flatplate_species.test_iter = 20
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turb_flatplate_species.test_vals = [-4.243064, -0.634797, -1.706652, 1.231264, -3.266203, 9.000000, -6.632972, 5.000000, -6.985977, 10.000000, -6.007208, 0.996237, 0.996237]
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test_list.append(turb_flatplate_species)
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# Flat plate SST compressibility correction Wilcox
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turb_flatplate_CC_Wilcox = TestCase('turb_flatplate_CC_Wilcox')
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turb_flatplate_CC_Wilcox.cfg_dir = "rans/flatplate"

‎TestCases/rans/flatplate/turb_SA_flatplate_species_ConstConductivity.cfg‎

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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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% %
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% SU2 configuration file %
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% Case description: Turbulent flow over flat plate with zero pressure gradient %
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% using conductivity model CONSTANT_CONDUCTIVITY %
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% Author: C. Morales Ubal %
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% Institution: Eindhoven University of Technology %
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% Date: 2025.02.22 %
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% File Version 8.1.0 "Harrier" %
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% %
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
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%
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SOLVER= RANS
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KIND_TURB_MODEL= SA
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MATH_PROBLEM= DIRECT
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RESTART_SOL= NO
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% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
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%
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MACH_NUMBER= 0.2
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AOA= 0.0
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SIDESLIP_ANGLE= 0.0
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FREESTREAM_TEMPERATURE= 300.0
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REYNOLDS_NUMBER= 5000000.0
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REYNOLDS_LENGTH= 1.0
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% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
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%
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REF_ORIGIN_MOMENT_X = 0.25
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REF_ORIGIN_MOMENT_Y = 0.00
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REF_ORIGIN_MOMENT_Z = 0.00
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REF_LENGTH= 1.0
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REF_AREA= 2.0
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% -------------------- FLUID PROPERTIES ------------------------------------- %
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%
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FLUID_MODEL= IDEAL_GAS
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%
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MOLECULAR_WEIGHT= 28.960
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%
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SPECIFIC_HEAT_CP = 1009.39
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%
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CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
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THERMAL_CONDUCTIVITY_CONSTANT= 0.0258
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%
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PRANDTL_LAM= 0.72
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TURBULENT_CONDUCTIVITY_MODEL= CONSTANT_PRANDTL_TURB
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PRANDTL_TURB= 0.90
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%
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% --------------------------- VISCOSITY MODEL ---------------------------------%
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%
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VISCOSITY_MODEL= CONSTANT_VISCOSITY
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%
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MU_CONSTANT= 1.8551E-05
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%
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% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
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%
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MARKER_HEATFLUX= ( wall, 0.0 )
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SPECIFIED_INLET_PROFILE= NO
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INLET_FILENAME= inlet.dat
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INC_INLET_TYPE= VELOCITY_INLET
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MARKER_INLET= ( inlet, 302.4, 118309.784, 1.0, 0.0, 0.0 )
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MARKER_INLET_SPECIES= ( inlet, 1.0 )
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MARKER_OUTLET= ( outlet, 115056.0, farfield, 115056.0 )
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MARKER_SYM= ( symmetry )
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MARKER_PLOTTING= ( wall )
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MARKER_MONITORING= ( wall )
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% -------------------- SCALAR TRANSPORT ---------------------------------------%
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%
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KIND_SCALAR_MODEL= SPECIES_TRANSPORT
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DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY
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DIFFUSIVITY_CONSTANT= 0.001
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CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
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MUSCL_SPECIES= NO
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SLOPE_LIMITER_SPECIES = NONE
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TIME_DISCRE_SPECIES= EULER_IMPLICIT
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SPECIES_INIT= 1.0
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SPECIES_CLIPPING= YES
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SPECIES_CLIPPING_MIN= 0.0
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SPECIES_CLIPPING_MAX= 1.0
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% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
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%
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NUM_METHOD_GRAD= GREEN_GAUSS
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CFL_NUMBER= 10.0
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CFL_ADAPT= YES
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CFL_ADAPT_PARAM= ( 0.5, 2.0, 1.0, 1000.0 )
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ITER= 10000
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% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
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%
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LINEAR_SOLVER= FGMRES
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LINEAR_SOLVER_PREC= ILU
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LINEAR_SOLVER_ERROR= 1E-5
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LINEAR_SOLVER_ITER= 5
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%
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% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
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%
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CONV_NUM_METHOD_FLOW= ROE
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MUSCL_FLOW= NO
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SLOPE_LIMITER_FLOW= NONE
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JST_SENSOR_COEFF= ( 0.5, 0.02 )
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TIME_DISCRE_FLOW= EULER_IMPLICIT
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% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
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%
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CONV_NUM_METHOD_TURB= SCALAR_UPWIND
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MUSCL_TURB= NO
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SLOPE_LIMITER_TURB= VENKATAKRISHNAN
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TIME_DISCRE_TURB= EULER_IMPLICIT
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% --------------------------- CONVERGENCE PARAMETERS --------------------------%
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CONV_RESIDUAL_MINVAL= -15
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CONV_STARTITER= 10
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CONV_CAUCHY_ELEMS= 100
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CONV_CAUCHY_EPS= 1E-6
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% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
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%
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MESH_FILENAME= mesh_flatplate_turb_137x97.su2
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SCREEN_OUTPUT= INNER_ITER WALL_TIME \
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RMS_DENSITY RMS_MOMENTUM-X RMS_MOMENTUM-Y RMS_ENERGY RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 \
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LINSOL_ITER LINSOL_RESIDUAL \
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LINSOL_ITER_TURB LINSOL_RESIDUAL_TURB \
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LINSOL_ITER_SPECIES LINSOL_RESIDUAL_SPECIES \
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SURFACE_SPECIES_0
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SCREEN_WRT_FREQ_INNER= 10
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HISTORY_OUTPUT= ITER RMS_RES LINSOL SPECIES_COEFF SPECIES_COEFF_SURF
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CONV_FILENAME= history
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MARKER_ANALYZE= outlet
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MARKER_ANALYZE_AVERAGE= AREA
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OUTPUT_FILES= RESTART_ASCII, PARAVIEW_MULTIBLOCK
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VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
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OUTPUT_WRT_FREQ= 100
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READ_BINARY_RESTART= NO
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RESTART_FILENAME= restart
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SOLUTION_FILENAME= solution
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