Sst consistency (#44)

pcarruscag · web-flow · commit 09e5662c3f30 · 2023-07-02T18:58:44.000-07:00
* set old SST version in configs

* fix name
diff --git a/compressible_flow/NICFD_nozzle/NICFD_nozzle.cfg b/compressible_flow/NICFD_nozzle/NICFD_nozzle.cfg
@@ -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
diff --git a/compressible_flow/Transitional_Airfoil/Langtry_and_Menter/E387/transitional_SST_LM_model_ConfigFile.cfg b/compressible_flow/Transitional_Airfoil/Langtry_and_Menter/E387/transitional_SST_LM_model_ConfigFile.cfg
@@ -14,6 +14,7 @@
 SOLVER= RANS
 %
 KIND_TURB_MODEL= SST
+SST_OPTIONS= V1994m
 KIND_TRANS_MODEL= LM
 FREESTREAM_TURBULENCEINTENSITY= 0.001
 %
diff --git a/compressible_flow/Transitional_Flat_Plate/Langtry_and_Menter/T3A-/transitional_LM_model_ConfigFile.cfg b/compressible_flow/Transitional_Flat_Plate/Langtry_and_Menter/T3A-/transitional_LM_model_ConfigFile.cfg
@@ -13,7 +13,7 @@ SOLVER= RANS
 %
 KIND_TURB_MODEL= SST
 %
-SST_OPTIONS= NONE
+SST_OPTIONS= V1994m
 KIND_TRANS_MODEL= LM
 %
 MATH_PROBLEM= DIRECT
diff --git a/compressible_flow/Transitional_Flat_Plate/Langtry_and_Menter/T3A/transitional_LM_model_ConfigFile.cfg b/compressible_flow/Transitional_Flat_Plate/Langtry_and_Menter/T3A/transitional_LM_model_ConfigFile.cfg
@@ -13,7 +13,7 @@ SOLVER= RANS
 %
 KIND_TURB_MODEL= SST
 %
-SST_OPTIONS= NONE
+SST_OPTIONS= V1994m
 KIND_TRANS_MODEL= LM
 %
 MATH_PROBLEM= DIRECT
diff --git a/incompressible_flow/Inc_Species_Transport/DAspecies3_primitiveVenturi.cfg b/incompressible_flow/Inc_Species_Transport/DAspecies3_primitiveVenturi.cfg
@@ -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];\
diff --git a/incompressible_flow/Inc_Species_Transport/species3_primitiveVenturi.cfg b/incompressible_flow/Inc_Species_Transport/species3_primitiveVenturi.cfg
@@ -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 -------------------%
 %
diff --git a/incompressible_flow/Inc_Species_Transport_Composition_Dependent_Model/kenics_mixer_tutorial.cfg b/incompressible_flow/Inc_Species_Transport_Composition_Dependent_Model/kenics_mixer_tutorial.cfg
@@ -16,6 +16,7 @@
 %
 SOLVER= INC_RANS
 KIND_TURB_MODEL= SST
+SST_OPTIONS= V1994m
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
diff --git a/incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_dp_hf_tp.cfg b/incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_dp_hf_tp.cfg
@@ -12,6 +12,7 @@
 %
 SOLVER= INC_RANS
 KIND_TURB_MODEL= SST
+SST_OPTIONS= V1994m
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %
diff --git a/incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_mf_hf.cfg b/incompressible_flow/Inc_Streamwise_Periodic/sp_pinArray_2d_mf_hf.cfg
@@ -12,6 +12,7 @@
 %
 SOLVER= INC_RANS
 KIND_TURB_MODEL= SST
+SST_OPTIONS= V1994m
 %
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
 %

Original file line number	Diff line number	Diff line change
`@@ -18,8 +18,9 @@`
`18`	`18`	`% POISSON_EQUATION)`
`19`	`19`	`SOLVER= RANS`
`20`	`20`	`%`
`21`		`-% Specify turbulence model (NONE, SA, SA_NEG, SST, SA_E, SA_COMP, SA_E_COMP)`
	`21`	`+% Specify turbulence model (NONE, SA, SST)`
`22`	`22`	`KIND_TURB_MODEL= SST`
	`23`	`+SST_OPTIONS= V1994m`
`23`	`24`	`%`
`24`	`25`	`% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)`
`25`	`26`	`MATH_PROBLEM= DIRECT`
Original file line number	Diff line number	Diff line change
`@@ -14,6 +14,7 @@`
`14`	`14`	`SOLVER= RANS`
`15`	`15`	`%`
`16`	`16`	`KIND_TURB_MODEL= SST`
	`17`	`+SST_OPTIONS= V1994m`
`17`	`18`	`KIND_TRANS_MODEL= LM`
`18`	`19`	`FREESTREAM_TURBULENCEINTENSITY= 0.001`
`19`	`20`	`%`
Original file line number	Diff line number	Diff line change
`@@ -13,7 +13,7 @@ SOLVER= RANS`
`13`	`13`	`%`
`14`	`14`	`KIND_TURB_MODEL= SST`
`15`	`15`	`%`
`16`		`-SST_OPTIONS= NONE`
	`16`	`+SST_OPTIONS= V1994m`
`17`	`17`	`KIND_TRANS_MODEL= LM`
`18`	`18`	`%`
`19`	`19`	`MATH_PROBLEM= DIRECT`
Original file line number	Diff line number	Diff line change
`@@ -13,6 +13,7 @@`
`13`	`13`	`%`
`14`	`14`	`SOLVER= INC_RANS`
`15`	`15`	`KIND_TURB_MODEL= SST`
	`16`	`+SST_OPTIONS= V1994m`
`16`	`17`	`%`
`17`	`18`	`CUSTOM_OUTPUTS= 'avg_species_0 : AreaAvg{SPECIES[0]}[outlet];\`
`18`	`19`	`avg_species_1 : AreaAvg{SPECIES[1]}[outlet];\`
Original file line number	Diff line number	Diff line change
`@@ -5,14 +5,15 @@`
`5`	`5`	`% Author: T. Kattmann %`
`6`	`6`	`% Institution: Bosch Thermotechniek B.V. %`
`7`	`7`	`% Date: 2021/10/14 %`
`8`		`-% File Version 7.2.1 "Blackbird" %`
	`8`	`+% File Version 7.5.1 "Blackbird" %`
`9`	`9`	`% %`
`10`	`10`	`%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%`
`11`	`11`
`12`	`12`	`% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%`
`13`	`13`	`%`
`14`	`14`	`SOLVER= INC_RANS`
`15`	`15`	`KIND_TURB_MODEL= SST`
	`16`	`+SST_OPTIONS= V1994m`
`16`	`17`	`%`
`17`	`18`	`% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%`
`18`	`19`	`%`
Original file line number	Diff line number	Diff line change
`@@ -16,6 +16,7 @@`
`16`	`16`	`%`
`17`	`17`	`SOLVER= INC_RANS`
`18`	`18`	`KIND_TURB_MODEL= SST`
	`19`	`+SST_OPTIONS= V1994m`
`19`	`20`	`%`
`20`	`21`	`% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%`
`21`	`22`	`%`
Original file line number	Diff line number	Diff line change
`@@ -12,6 +12,7 @@`
`12`	`12`	`%`
`13`	`13`	`SOLVER= INC_RANS`
`14`	`14`	`KIND_TURB_MODEL= SST`
	`15`	`+SST_OPTIONS= V1994m`
`15`	`16`	`%`
`16`	`17`	`% ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%`
`17`	`18`	`%`