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add keyword and testcase
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‎Common/src/CConfig.cpp‎

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@@ -1627,6 +1627,10 @@ void CConfig::SetConfig_Options() {
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/*!\brief MARKER_RIEMANN \n DESCRIPTION: Riemann boundary marker(s) with the following formats, a unit vector.
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* \n OPTIONS: See \link Riemann_Map \endlink. The variables indicated by the option and the flow direction unit vector must be specified. \ingroup Config*/
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addRiemannOption("MARKER_RIEMANN", nMarker_Riemann, Marker_Riemann, Kind_Data_Riemann, Riemann_Map, Riemann_Var1, Riemann_Var2, Riemann_FlowDir);
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/*!\brief MARKER_WALL_SPECIES \n DESCRIPTION: Wall species boundary marker(s) with the following format:
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* (marker_name, BC_TYPE, value, ...) where BC_TYPE is either FLUX (Neumann) or VALUE (Dirichlet).
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* \n OPTIONS: See \link Wall_Map \endlink. \ingroup Config*/
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addWallSpeciesOption("MARKER_WALL_SPECIES", nMarker_Wall_Species, Marker_Wall_Species, Kind_Wall_Species, Wall_Map, Wall_SpeciesVal);
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/*!\brief MARKER_GILES \n DESCRIPTION: Giles boundary marker(s) with the following formats, a unit vector. */
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/* \n OPTIONS: See \link Giles_Map \endlink. The variables indicated by the option and the flow direction unit vector must be specified. \ingroup Config*/
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addGilesOption("MARKER_GILES", nMarker_Giles, Marker_Giles, Kind_Data_Giles, Giles_Map, Giles_Var1, Giles_Var2, Giles_FlowDir, RelaxFactorAverage, RelaxFactorFourier);

‎TestCases/species_transport/venturi_primitive_3species/species2_primitiveVenturi_flux_value.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 2 species, i.e. 1 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 8.3.0 "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= INC_RANS
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KIND_TURB_MODEL= SST
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%
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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_INIT= 1.1766
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%
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INC_VELOCITY_INIT= ( 1.00, 0.0, 0.0 )
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%
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INC_ENERGY_EQUATION= YES
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INC_TEMPERATURE_INIT= 300.0
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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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%
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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= CONSTANT_VISCOSITY
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MU_CONSTANT= 1.716E-5
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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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MARKER_SYM= ( axis )
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%
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INC_INLET_TYPE= VELOCITY_INLET VELOCITY_INLET
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MARKER_INLET= ( gas_inlet, 300, 1.0, 1.0, 0.0, 0.0,\
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air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
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MARKER_INLET_SPECIES= (gas_inlet, 0.1,\
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air_axial_inlet, 0.0 )
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MARKER_WALL_SPECIES=(axis,FLUX,0.1,wall,VALUE,0.5)
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%
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INC_OUTLET_TYPE= PRESSURE_OUTLET
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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= 60
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CFL_REDUCTION_SPECIES= 1.0
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CFL_REDUCTION_TURB= 1.0
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%
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ITER= 10
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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-8
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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= FDS
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MUSCL_FLOW= YES
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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_DIFFUSIVITY
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DIFFUSIVITY_CONSTANT= 0.001
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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= 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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%
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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= primitiveVenturi.su2
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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 \
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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 SURFACE_SPECIES_VARIANCE
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SCREEN_WRT_FREQ_INNER= 10
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%
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HISTORY_OUTPUT= RMS_RES FLOW_COEFF LINSOL SPECIES_COEFF SPECIES_COEFF_SURF
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MARKER_ANALYZE= outlet gas_inlet air_axial_inlet
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%
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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= 1000
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%
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RESTART_SOL= NO
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SOLUTION_FILENAME= solution
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RESTART_FILENAME= restart
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%
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WRT_PERFORMANCE= YES

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