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Merged
pcarruscag merged 3 commits into from
Apr 30, 2023
Merged

Avoid duplicated config that is already in the code repo #41

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2ec2880
remove config since it is in the code repo
pcarruscag Apr 30, 2023
4672749
Revert "remove config since it is in the code repo"
pcarruscag Apr 30, 2023
c16c67e
use the config in tutorials instead
pcarruscag Apr 30, 2023
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Revert "remove config since it is in the code repo" 
This reverts commit 2ec2880.
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@pcarruscag
pcarruscag committed Apr 30, 2023
commit 46727496bfd371fb7e28b85e80fd54d0471a5424
142 changes: 142 additions & 0 deletions incompressible_flow/Inc_Species_Transport/DAspecies3_primitiveVenturi.cfg
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
% %
% SU2 configuration file %
% Case description: Discrete Adjiont Species mixing with 3 species %
% Author: T. Kattmann %
% Institution: Bosch Thermotechniek B.V. %
% Date: 2021/10/14 %
% File Version 7.2.1 "Blackbird" %
% %
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
%
SOLVER= INC_RANS
KIND_TURB_MODEL= SST
%
OBJECTIVE_FUNCTION= SURFACE_SPECIES_VARIANCE
OBJECTIVE_WEIGHT= 1.0
%
% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
%
INC_DENSITY_MODEL= CONSTANT
INC_DENSITY_INIT= 1.1766
%
INC_VELOCITY_INIT= ( 1.00, 0.0, 0.0 )
%
INC_ENERGY_EQUATION= YES
INC_TEMPERATURE_INIT= 300.0
%
INC_NONDIM= INITIAL_VALUES
%
% -------------------- FLUID PROPERTIES ------------------------------------- %
%
FLUID_MODEL= CONSTANT_DENSITY
%
CONDUCTIVITY_MODEL= CONSTANT_CONDUCTIVITY
THERMAL_CONDUCTIVITY_CONSTANT= 0.0357
%
PRANDTL_LAM= 0.72
TURBULENT_CONDUCTIVITY_MODEL= NONE
PRANDTL_TURB= 0.90
%
VISCOSITY_MODEL= CONSTANT_VISCOSITY
MU_CONSTANT= 1.716E-5
%
% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
%
MARKER_HEATFLUX= ( wall, 0.0 )
MARKER_SYM= ( axis )
%
SPECIFIED_INLET_PROFILE= NO
INLET_FILENAME= inlet_venturi.dat
INC_INLET_TYPE= VELOCITY_INLET VELOCITY_INLET
MARKER_INLET= ( gas_inlet, 300, 1.0, 1.0, 0.0, 0.0,\
air_axial_inlet, 300, 1.0, 0.0, -1.0, 0.0 )
SPECIES_USE_STRONG_BC= NO
MARKER_INLET_SPECIES= (gas_inlet, 0.5, 0.5,\
air_axial_inlet, 0.6, 0.0 )
%
INC_OUTLET_TYPE= PRESSURE_OUTLET
MARKER_OUTLET= ( outlet, 0.0 )
%
% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
%
NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
%
% Note that the CFL-Number was dramatically reduced compared to the primal.
% This was necessary to ensure proper convergence. It is not necessary to do
% this for a reasonably accurate gradient validation though.
CFL_NUMBER= 500
CFL_REDUCTION_SPECIES= 1.0
CFL_REDUCTION_TURB= 1.0
%
% Run commented Iter for good results
ITER= 50
%
% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
%
LINEAR_SOLVER= FGMRES
LINEAR_SOLVER_PREC= ILU
LINEAR_SOLVER_ERROR= 1E-8
LINEAR_SOLVER_ITER= 20

% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
%
CONV_NUM_METHOD_FLOW= FDS
MUSCL_FLOW= YES
SLOPE_LIMITER_FLOW = NONE
TIME_DISCRE_FLOW= EULER_IMPLICIT
%
% -------------------- SCALAR TRANSPORT ---------------------------------------%
%
KIND_SCALAR_MODEL= SPECIES_TRANSPORT
DIFFUSIVITY_MODEL= CONSTANT_DIFFUSIVITY
DIFFUSIVITY_CONSTANT= 0.001
%
CONV_NUM_METHOD_SPECIES= SCALAR_UPWIND
MUSCL_SPECIES= NO
SLOPE_LIMITER_SPECIES = NONE
%
TIME_DISCRE_SPECIES= EULER_IMPLICIT
%
SPECIES_INIT= 1.0, 0.0
SPECIES_CLIPPING= YES
SPECIES_CLIPPING_MIN= 0.0, 0.0
SPECIES_CLIPPING_MAX= 1.0, 1.0
%
% -------------------- TURBULENT TRANSPORT ---------------------------------------%
%
CONV_NUM_METHOD_TURB= SCALAR_UPWIND
MUSCL_TURB= NO
%
% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
CONV_FIELD= RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCITY-Y, RMS_TKE, RMS_SPECIES
CONV_RESIDUAL_MINVAL= -18
CONV_STARTITER= 10
%
% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
%
MESH_FILENAME= primitiveVenturi.su2
%
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
SCREEN_WRT_FREQ_INNER= 10
%
HISTORY_OUTPUT= ITER RMS_RES LINSOL
CONV_FILENAME= history
MARKER_ANALYZE= outlet
MARKER_ANALYZE_AVERAGE= MASSFLUX
%
OUTPUT_FILES= RESTART_ASCII, PARAVIEW_MULTIBLOCK
VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
OUTPUT_WRT_FREQ= 1000
%
GRAD_OBJFUNC_FILENAME= of_grad.csv
%
RESTART_SOL= NO
READ_BINARY_RESTART= NO
RESTART_FILENAME= restart
SOLUTION_FILENAME= solution
%
WRT_PERFORMANCE= YES