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Revert "remove config since it is in the code repo"
This reverts commit 2ec2880.
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‎incompressible_flow/Inc_Species_Transport/DAspecies3_primitiveVenturi.cfg‎

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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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% %
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% SU2 configuration file %
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% Case description: Discrete Adjiont Species mixing with 3 species %
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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 7.2.1 "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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%
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OBJECTIVE_FUNCTION= SURFACE_SPECIES_VARIANCE
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OBJECTIVE_WEIGHT= 1.0
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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= INITIAL_VALUES
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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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SPECIFIED_INLET_PROFILE= NO
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INLET_FILENAME= inlet_venturi.dat
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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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SPECIES_USE_STRONG_BC= NO
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MARKER_INLET_SPECIES= (gas_inlet, 0.5, 0.5,\
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air_axial_inlet, 0.6, 0.0 )
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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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% Note that the CFL-Number was dramatically reduced compared to the primal.
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% This was necessary to ensure proper convergence. It is not necessary to do
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% this for a reasonably accurate gradient validation though.
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CFL_NUMBER= 500
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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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% Run commented Iter for good results
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ITER= 50
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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= 20
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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= SCALAR_UPWIND
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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, 0.0
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SPECIES_CLIPPING= YES
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SPECIES_CLIPPING_MIN= 0.0, 0.0
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SPECIES_CLIPPING_MAX= 1.0, 1.0
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%
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% -------------------- TURBULENT TRANSPORT ---------------------------------------%
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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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%
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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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%
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SCREEN_OUTPUT= INNER_ITER WALL_TIME RMS_ADJ_PRESSURE RMS_ADJ_VELOCITY-X RMS_ADJ_VELOCITY-Y RMS_ADJ_TKE RMS_ADJ_DISSIPATION RMS_ADJ_SPECIES_0 RMS_ADJ_SPECIES_1
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SCREEN_WRT_FREQ_INNER= 10
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%
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HISTORY_OUTPUT= ITER RMS_RES LINSOL
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CONV_FILENAME= history
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MARKER_ANALYZE= outlet
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MARKER_ANALYZE_AVERAGE= MASSFLUX
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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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GRAD_OBJFUNC_FILENAME= of_grad.csv
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%
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RESTART_SOL= NO
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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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