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add testcases
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‎TestCases/py_wrapper/psi_heatloss/psi.cfg‎

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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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% %
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% SU2 configuration file %
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% Case description: Species mixing with 3 species, i.e. 2 transport equations %
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% Author: T. Kattmann %
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% Institution: Bosch Thermotechniek B.V. %
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% Date: 2021/10/14 %
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% File Version 7.5.1 "Blackbird" %
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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= INC_RANS
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KIND_TURB_MODEL= SST
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SST_OPTIONS= V2003m
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RESTART_SOL= YES
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MGLEVEL= 0
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%
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% temperature and density
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FREESTREAM_TEMPERATURE = 673
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FREESTREAM_DENSITY = 2.50
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% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
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%
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%INC_DENSITY_MODEL= CONSTANT
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INC_DENSITY_MODEL= VARIABLE
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INC_DENSITY_INIT= 2.50
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%
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INC_VELOCITY_INIT= (40.00, 0.0, 0.0 )
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%
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INC_ENERGY_EQUATION= YES
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INC_TEMPERATURE_INIT= 673.0
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%
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INC_NONDIM= DIMENSIONAL
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%
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% -------------------- FLUID PROPERTIES ------------------------------------- %
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%
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%FLUID_MODEL= CONSTANT_DENSITY
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FLUID_MODEL= INC_IDEAL_GAS
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%
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CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
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THERMAL_CONDUCTIVITY_CONSTANT= 0.0357
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%
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PRANDTL_LAM= 0.72
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TURBULENT_CONDUCTIVITY_MODEL= NONE
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PRANDTL_TURB= 0.90
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%
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VISCOSITY_MODEL= SUTHERLAND
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MU_CONSTANT= 1.716E-5
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MU_REF = 1.716e-5
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MU_T_REF= 273.15
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SUTHERLAND_CONSTANT = 110.4
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SPECIFIC_HEAT_CP = 1150
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%
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% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
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%
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MARKER_HEATFLUX= ( wall_pipe,0.0, wall_interior, 0.0,wall_top, 0,wall_side,0 )
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% note, case is axisymmetric
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MARKER_SYM= ( symmetry )
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AXISYMMETRIC= YES
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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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INC_INLET_DAMPING= 0.01
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MARKER_INLET= ( inlet, 673, 40.0, 1.0, 0.0, 0.0)
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MARKER_INLET_TURBULENT = (inlet, 0.10, 15)
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MARKER_INLET_SPECIES= (inlet, 0.0, 304721)
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INLET_MATCHING_TOLERANCE = 1e-3
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MARKER_PYTHON_CUSTOM= (wall_top)
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MARKER_WALL_SPECIES= wall_side, FLUX,0,VALUE,304721, wall_pipe, FLUX,0 , VALUE,304721 ,wall_interior , FLUX,0 , VALUE,304721 ,wall_top, FLUX,0,VALUE,-250000
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MARKER_SPECIES_STRONG_BC=wall_top,wall_side,wall_pipe,wall_interior
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%
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INC_OUTLET_TYPE= PRESSURE_OUTLET
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INC_OUTLET_DAMPING= 0.01
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MARKER_OUTLET= ( outlet, 0.0 )
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%
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% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
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%
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NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
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%
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%CFL_NUMBER= 25.0
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CFL_NUMBER= 10.0
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CFL_REDUCTION_SPECIES= 1.0
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CFL_REDUCTION_TURB= 1.0
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CFL_ADAPT= NO
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CFL_ADAPT_PARAM= ( 0.95, 1.01, 1.0, 250, 1.0e-4, 0)
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%
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% Run commented Iter for good results
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ITER= 1
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%
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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-10
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LINEAR_SOLVER_ITER= 10
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% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
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%
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CONV_NUM_METHOD_FLOW= FDS
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MUSCL_FLOW= NO
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SLOPE_LIMITER_FLOW = NONE
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TIME_DISCRE_FLOW= EULER_IMPLICIT
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%
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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_SCHMIDT
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DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY
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SCHMIDT_NUMBER_LAMINAR= 0.5
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DIFFUSIVITY_CONSTANT= 0.000148
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% according to the paper
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SCHMIDT_NUMBER_TURBULENT= 0.7
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%
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CONV_NUM_METHOD_SPECIES= BOUNDED_SCALAR
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MUSCL_SPECIES= NO
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SLOPE_LIMITER_SPECIES = NONE
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%
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TIME_DISCRE_SPECIES= EULER_IMPLICIT
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%
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SPECIES_INIT= 0.0, 200000
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SPECIES_CLIPPING= NO
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SPECIES_CLIPPING_MIN= 0.0, -1.5e+6
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SPECIES_CLIPPING_MAX= 1.0, 304721
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%
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% -------------------- TURBULENT TRANSPORT ---------------------------------------%
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%
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CONV_NUM_METHOD_TURB= BOUNDED_SCALAR
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MUSCL_TURB= NO
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%
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% --------------------------- CONVERGENCE PARAMETERS --------------------------%
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%
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CONV_FIELD= RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_TKE, RMS_SPECIES
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CONV_RESIDUAL_MINVAL= -18
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CONV_STARTITER= 10
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%
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% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
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%
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MESH_FILENAME= psi.su2
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%MESH_FILENAME= psi_medium.su2
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%MESH_FILENAME= psi_fine.su2
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%
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SCREEN_OUTPUT= INNER_ITER WALL_TIME \
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RMS_PRESSURE RMS_VELOCITY-X RMS_VELOCITY-Y RMS_TKE RMS_DISSIPATION RMS_SPECIES_0 RMS_SPECIES_1 \
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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= 1
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%
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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= gas_inlet, air_axial_inlet, outlet
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MARKER_ANALYZE_AVERAGE= AREA
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%
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OUTPUT_FILES= RESTART_ASCII, PARAVIEW_MULTIBLOCK
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VOLUME_OUTPUT= RESIDUAL, PRIMITIVE, RANK, SPECIES_UDS_0
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OUTPUT_WRT_FREQ= 100
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%
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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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%
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WRT_PERFORMANCE= YES
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PYTHON_CUSTOM_SOURCE= YES

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