Update other NACA 0012 RANS configs to use binary restart

bmunguia · bmunguia · commit 9ffa8ecf6e5d · 2025-10-23T09:31:26.000-07:00
diff --git a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg
@@ -17,7 +17,6 @@ SST_OPTIONS= V1994m
 KIND_TURB_MODEL= SST
 MATH_PROBLEM= DISCRETE_ADJOINT
 RESTART_SOL= NO
-READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_1994-KLm.cfg
@@ -14,7 +14,6 @@ KIND_TURB_MODEL= SST
 SST_OPTIONS= (V1994m ,KATO-LAUNDER)
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
-READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
@@ -104,4 +103,4 @@ SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 10000
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL)
-OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW)
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_2003-Vm.cfg
@@ -14,7 +14,6 @@ KIND_TURB_MODEL= SST
 SST_OPTIONS= (V2003m ,VORTICITY)
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
-READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
@@ -104,4 +103,4 @@ SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 10000
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL)
-OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW)
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_2003m.cfg
@@ -11,7 +11,6 @@ SOLVER= RANS
 KIND_TURB_MODEL= SST
 SST_OPTIONS= V2003m
 RESTART_SOL= YES
-READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_expliciteuler.cfg
@@ -14,15 +14,14 @@ SOLVER= RANS
 KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
 RESTART_SOL= NO
-READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 MACH_NUMBER= 0.15
 AOA= 10.0
 FREESTREAM_TEMPERATURE= 300.0
 REYNOLDS_NUMBER= 6.0E6
 REYNOLDS_LENGTH= 1.0
- 
+
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
 REF_LENGTH= 1.0
 REF_AREA= 1.0
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_fixedvalues.cfg
@@ -14,7 +14,6 @@ SOLVER= RANS
 KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
 RESTART_SOL= NO
-READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 MACH_NUMBER= 0.15
@@ -86,4 +85,4 @@ VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
 OUTPUT_WRT_FREQ= 10000
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL)
-OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW)
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_multigrid_restart.cfg
@@ -6,7 +6,7 @@
 % Author: David E. Manosalvas                                                  %
 % Institution: Stanford University                                             %
 % Date: 02.14.2017                                                             %
-% File Version 8.3.0 "Harrier"                                                 %
+% File Version 8.2.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -16,11 +16,8 @@ SOLVER= RANS
 KIND_TURB_MODEL= SST
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
-READ_BINARY_RESTART= NO
 DISCARD_INFILES= YES
 SYSTEM_MEASUREMENTS= SI
-GRAVITY_FORCE= NO
-AXISYMMETRIC= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
@@ -125,7 +122,7 @@ CFL_REDUCTION_ADJFLOW= 0.8
 LIMIT_ADJFLOW= 1E6
 
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
-ITER= 100
+ITER= 999
 CONV_RESIDUAL_MINVAL= -12
 CONV_STARTITER= 30
 CONV_CAUCHY_ELEMS= 500
@@ -135,17 +132,17 @@ CONV_CAUCHY_EPS= 1E-6
 %
 MESH_FILENAME= n0012_113-33.su2
 MESH_FORMAT= SU2
-MESH_OUT_FILENAME= mesh_out
-SOLUTION_FILENAME= solution_flow_sst_restart
-SOLUTION_ADJ_FILENAME= solution_adj
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow_sst_restart.dat
+SOLUTION_ADJ_FILENAME= solution_adj.dat
 TABULAR_FORMAT= CSV
 CONV_FILENAME= history
-RESTART_FILENAME= restart_flow
-RESTART_ADJ_FILENAME= restart_adj
+RESTART_FILENAME= restart_flow.dat
+RESTART_ADJ_FILENAME= restart_adj.dat
 VOLUME_FILENAME= flow
 VOLUME_ADJ_FILENAME= adjoint
-VALUE_OBJFUNC_FILENAME= of_eval
-GRAD_OBJFUNC_FILENAME= of_grad
+VALUE_OBJFUNC_FILENAME= of_eval.dat
+GRAD_OBJFUNC_FILENAME= of_grad.dat
 SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 OUTPUT_WRT_FREQ= 500
diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg
@@ -6,7 +6,7 @@
 % Author: Thomas D. Economon                                                   %
 % Institution: Stanford University                                             %
 % Date: Feb 18th, 2013                                                         %
-% File Version 8.3.0 "Harrier"                                                 %
+% File Version 8.2.0 "Harrier"                                                 %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -17,7 +17,6 @@ KIND_TURB_MODEL= SST
 SST_OPTIONS=(SUSTAINING)
 MATH_PROBLEM= DIRECT
 RESTART_SOL= YES
-READ_BINARY_RESTART= NO
 
 % -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
 %
@@ -88,13 +87,13 @@ CONV_CAUCHY_EPS= 1E-6
 %
 MESH_FILENAME= n0012_225-65.su2
 MESH_FORMAT= SU2
-MESH_OUT_FILENAME= mesh_out
-SOLUTION_FILENAME= solution_flow_sst_sust
+MESH_OUT_FILENAME= mesh_out.su2
+SOLUTION_FILENAME= solution_flow_sst_sust.dat
 TABULAR_FORMAT= CSV
 CONV_FILENAME= history
-RESTART_FILENAME= restart_flow
+RESTART_FILENAME= restart_flow.dat
 VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
 OUTPUT_WRT_FREQ= 10000
 SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, LINSOL_RESIDUAL)
-OUTPUT_FILES= (RESTART_ASCII, PARAVIEW, SURFACE_PARAVIEW)
+OUTPUT_FILES= (RESTART, PARAVIEW, SURFACE_PARAVIEW)

Original file line number	Diff line number	Diff line change
`@@ -17,7 +17,6 @@ SST_OPTIONS= V1994m`
`17`	`17`	`KIND_TURB_MODEL= SST`
`18`	`18`	`MATH_PROBLEM= DISCRETE_ADJOINT`
`19`	`19`	`RESTART_SOL= NO`
`20`		`-READ_BINARY_RESTART= NO`
`21`	`20`
`22`	`21`	`% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%`
`23`	`22`	`%`
Original file line number	Diff line number	Diff line change
`@@ -11,7 +11,6 @@ SOLVER= RANS`
`11`	`11`	`KIND_TURB_MODEL= SST`
`12`	`12`	`SST_OPTIONS= V2003m`
`13`	`13`	`RESTART_SOL= YES`
`14`		`-READ_BINARY_RESTART= NO`
`15`	`14`
`16`	`15`	`% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%`
`17`	`16`	`%`