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Sst consistency #44

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Merged
pcarruscag merged 2 commits into from
Jul 3, 2023
Merged

Sst consistency #44

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5607cc5
set old SST version in configs
pcarruscag Jul 1, 2023
2f22bb6
fix name
pcarruscag Jul 1, 2023
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3 changes: 2 additions & 1 deletion compressible_flow/NICFD_nozzle/NICFD_nozzle.cfg
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Expand Up @@ -18,8 +18,9 @@
% POISSON_EQUATION)
SOLVER= RANS
%
% Specify turbulence model (NONE, SA, SA_NEG, SST, SA_E, SA_COMP, SA_E_COMP)
% Specify turbulence model (NONE, SA, SST)
KIND_TURB_MODEL= SST
SST_OPTIONS= V1994m
%
% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
MATH_PROBLEM= DIRECT
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1 change: 1 addition & 0 deletions ...low/Transitional_Airfoil/Langtry_and_Menter/E387/transitional_SST_LM_model_ConfigFile.cfg
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Expand Up @@ -14,6 +14,7 @@
SOLVER= RANS
%
KIND_TURB_MODEL= SST
SST_OPTIONS= V1994m
KIND_TRANS_MODEL= LM
FREESTREAM_TURBULENCEINTENSITY= 0.001
%
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2 changes: 1 addition & 1 deletion ...flow/Transitional_Flat_Plate/Langtry_and_Menter/T3A-/transitional_LM_model_ConfigFile.cfg
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Expand Up @@ -13,7 +13,7 @@ SOLVER= RANS
%
KIND_TURB_MODEL= SST
%
SST_OPTIONS= NONE
SST_OPTIONS= V1994m
KIND_TRANS_MODEL= LM
%
MATH_PROBLEM= DIRECT
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2 changes: 1 addition & 1 deletion ..._flow/Transitional_Flat_Plate/Langtry_and_Menter/T3A/transitional_LM_model_ConfigFile.cfg
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Expand Up @@ -13,7 +13,7 @@ SOLVER= RANS
%
KIND_TURB_MODEL= SST
%
SST_OPTIONS= NONE
SST_OPTIONS= V1994m
KIND_TRANS_MODEL= LM
%
MATH_PROBLEM= DIRECT
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1 change: 1 addition & 0 deletions incompressible_flow/Inc_Species_Transport/DAspecies3_primitiveVenturi.cfg
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Expand Up @@ -13,6 +13,7 @@
%
SOLVER= INC_RANS
KIND_TURB_MODEL= SST
SST_OPTIONS= V1994m
%
CUSTOM_OUTPUTS= 'avg_species_0 : AreaAvg{SPECIES[0]}[outlet];\
avg_species_1 : AreaAvg{SPECIES[1]}[outlet];\
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3 changes: 2 additions & 1 deletion incompressible_flow/Inc_Species_Transport/species3_primitiveVenturi.cfg
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Expand Up @@ -5,14 +5,15 @@
% Author: T. Kattmann %
% Institution: Bosch Thermotechniek B.V. %
% Date: 2021/10/14 %
% File Version 7.2.1 "Blackbird" %
% File Version 7.5.1 "Blackbird" %
% %
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
%
SOLVER= INC_RANS
KIND_TURB_MODEL= SST
SST_OPTIONS= V1994m
%
% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
%
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1 change: 1 addition & 0 deletions ...ressible_flow/Inc_Species_Transport_Composition_Dependent_Model/kenics_mixer_tutorial.cfg
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Expand Up @@ -16,6 +16,7 @@
%
SOLVER= INC_RANS
KIND_TURB_MODEL= SST
SST_OPTIONS= V1994m
%
% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
%
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1 change: 1 addition & 0 deletions incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_dp_hf_tp.cfg
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Expand Up @@ -12,6 +12,7 @@
%
SOLVER= INC_RANS
KIND_TURB_MODEL= SST
SST_OPTIONS= V1994m
%
% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
%
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1 change: 1 addition & 0 deletions incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_mf_hf.cfg
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Expand Up @@ -12,6 +12,7 @@
%
SOLVER= INC_RANS
KIND_TURB_MODEL= SST
SST_OPTIONS= V1994m
%
% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
%
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