Update cfg files. Cleaning + formatting.

Author: TobiKattmann

TestCases/wallfunctions/flatplate/compressible_SA/turb_SA_flatplate.cfg

@@ -1,38 +1,48 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file                                                       %
-% Case description: Turbulent flow over flat plate, wall functions             %
-% Author: Nijso Beishuizen                                                     %
+% Case description: Comp. turbulent flow over flat plate, wall functions       %
+%                   https://turbmodels.larc.nasa.gov/flatplate_sa.html         %
+% Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
 % File Version 7.2.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
+%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
 SOLVER= RANS
 KIND_TURB_MODEL= SA
-MATH_PROBLEM= DIRECT
-RESTART_SOL= NO 
+RESTART_SOL= NO
+%
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
-MACH_NUMBER= 0.2
+%
 FREESTREAM_TEMPERATURE= 300.0
+MACH_NUMBER= 0.2
 REYNOLDS_NUMBER= 5e6
 REYNOLDS_LENGTH= 1.0
+%
 % --------------------------- VISCOSITY MODEL ---------------------------------%
+%
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 % NOTE check where the material conditions come from https://turbmodels.larc.nasa.gov/flatplate.html ... is this even active
 MU_CONSTANT= 1.8573E-5
+%
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_DIMENSIONALIZATION= DIMENSIONAL
 REF_LENGTH= 1.0
 REF_AREA= 2.0
+%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
 MARKER_HEATFLUX= ( wall, 0.0 )
+MARKER_SYM= ( symmetry )
+%
 MARKER_INLET= ( inlet, 302.4, 118309.784, 1.0, 0.0, 0.0 )
 MARKER_OUTLET= ( outlet, 115056.0, farfield, 115056.0 )
-MARKER_SYM= ( symmetry )
-MARKER_PLOTTING= ( wall )
-MARKER_MONITORING= ( wall )
+%
 % ------------------------ WALL FUNCTION DEFINITION --------------------------%
 %
 MARKER_WALL_FUNCTIONS= ( wall, STANDARD_WALL_FUNCTION )
@@ -43,10 +53,12 @@ WALLMODEL_MAXITER= 200
 WALLMODEL_RELFAC= 0.5
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
 NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 1e3
 CFL_ADAPT= NO
 ITER= 1000
+%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= FGMRES
@@ -55,22 +67,30 @@ LINEAR_SOLVER_ERROR= 1e-15
 LINEAR_SOLVER_ITER= 10
 %
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
 MGLEVEL= 0
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
 CONV_NUM_METHOD_FLOW= ROE
 MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW= NONE
 TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
 MUSCL_TURB= NO
 SLOPE_LIMITER_TURB= NONE
 TIME_DISCRE_TURB= EULER_IMPLICIT
+%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
 CONV_RESIDUAL_MINVAL= -15
 CONV_STARTITER= 10
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
+%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= ../mesh_flatplate_140x100.su2
@@ -81,7 +101,9 @@ SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM
 SCREEN_WRT_FREQ_INNER= 10
 %
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, FLOW_COEFF)
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
 %
 OUTPUT_FILES= RESTART, PARAVIEW_MULTIBLOCK
-VOLUME_OUTPUT= RESIDUAL, PRIMITIVE
+VOLUME_OUTPUT= RESIDUAL, PRIMITIVE, RESIDUAL
 OUTPUT_WRT_FREQ= 1000

TestCases/wallfunctions/flatplate/compressible_SST/turb_SST_flatplate.cfg

@@ -1,38 +1,48 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file                                                       %
-% Case description: Turbulent flow over flat plate, wall functions             %
-% Author: Nijso Beishuizen                                                     %
+% Case description: Comp. turbulent flow over flat plate, wall functions       %
+%                   https://turbmodels.larc.nasa.gov/flatplate_sa.html         %
+% Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
 % File Version 7.2.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
+%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
 SOLVER= RANS
 KIND_TURB_MODEL= SST
-MATH_PROBLEM= DIRECT
-RESTART_SOL= NO 
+RESTART_SOL= NO
+%
 % ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
-MACH_NUMBER= 0.2
+%
 FREESTREAM_TEMPERATURE= 300.0
-REYNOLDS_NUMBER= 5000000.0
+MACH_NUMBER= 0.2
+REYNOLDS_NUMBER= 5e6
 REYNOLDS_LENGTH= 1.0
+%
 % --------------------------- VISCOSITY MODEL ---------------------------------%
+%
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 % NOTE check where the material conditions come from https://turbmodels.larc.nasa.gov/flatplate.html ... is this even active
 MU_CONSTANT= 1.8573E-5
+%
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+REF_DIMENSIONALIZATION= DIMENSIONAL
 REF_LENGTH= 1.0
 REF_AREA= 2.0
+%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
 MARKER_HEATFLUX= ( wall, 0.0 )
+MARKER_SYM= ( symmetry )
+%
 MARKER_INLET= ( inlet, 302.4, 118309.784, 1.0, 0.0, 0.0 )
 MARKER_OUTLET= ( outlet, 115056.0, farfield, 115056.0 )
-MARKER_SYM= ( symmetry )
-MARKER_PLOTTING= ( wall )
-MARKER_MONITORING= ( wall )
+%
 % ------------------------ WALL FUNCTION DEFINITION --------------------------%
 %
 MARKER_WALL_FUNCTIONS= ( wall, STANDARD_WALL_FUNCTION )
@@ -43,10 +53,12 @@ WALLMODEL_MAXITER= 200
 WALLMODEL_RELFAC= 0.5
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
 NUM_METHOD_GRAD= GREEN_GAUSS
-CFL_NUMBER= 400.0
+CFL_NUMBER= 4e2
 CFL_ADAPT= NO
 ITER= 2000
+%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= FGMRES
@@ -55,22 +67,30 @@ LINEAR_SOLVER_ERROR= 1e-15
 LINEAR_SOLVER_ITER= 10
 %
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
 MGLEVEL= 0
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
 CONV_NUM_METHOD_FLOW= ROE
 MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW= NONE
 TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
 MUSCL_TURB= NO
 SLOPE_LIMITER_TURB= NONE
 TIME_DISCRE_TURB= EULER_IMPLICIT
+%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
+%
 CONV_RESIDUAL_MINVAL= -15
 CONV_STARTITER= 10
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
+%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= ../mesh_flatplate_140x100.su2
@@ -81,7 +101,9 @@ SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_DENSITY, RMS_MOMENTUM-X, RMS_MOMENTUM
 SCREEN_WRT_FREQ_INNER= 10
 %
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, FLOW_COEFF)
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
 %
 OUTPUT_FILES= RESTART, PARAVIEW_MULTIBLOCK
-VOLUME_OUTPUT= RESIDUAL
+VOLUME_OUTPUT= RESIDUAL, PRIMITIVE, RESIDUAL
 OUTPUT_WRT_FREQ= 1000

TestCases/wallfunctions/flatplate/incompressible_SA/turb_SA_flatplate.cfg

@@ -1,45 +1,51 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %                                                                              %
 % SU2 configuration file                                                       %
-% Case description: Turbulent flow over flat plate, wall functions             %
-% Author: Nijso Beishuizen                                                     %
+% Case description: Incomp. turbulent flow over flat plate, wall functions     %
+%                   https://turbmodels.larc.nasa.gov/flatplate_sa.html         %
+% Author: Nijso Beishuizen, T. Kattmann                                        %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 2021.09.01                                                             %
 % File Version 7.2.0 "Blackbird"                                               %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
-
+%
 % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
+%
 SOLVER= INC_RANS
 KIND_TURB_MODEL= SA
-MATH_PROBLEM= DIRECT
-RESTART_SOL= NO 
+RESTART_SOL= NO
+%
 % ---------------- INCOMPRESSIBLE FLOW CONDITION DEFINITION -------------------%
+%
 INC_DENSITY_MODEL= CONSTANT
 INC_DENSITY_INIT= 1.3254
 INC_ENERGY_EQUATION= YES
 INC_TEMPERATURE_INIT= 300.00
 INC_VELOCITY_INIT= (70, 0.0, 0.0 )
+%
 % --------------------------- VISCOSITY MODEL ---------------------------------%
+%
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 MU_CONSTANT= 1.8573E-5
-% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
-MACH_NUMBER= 0.2
-FREESTREAM_TEMPERATURE= 300.0
-REYNOLDS_NUMBER= 5000000.0
-REYNOLDS_LENGTH= 1.0
+%
 % ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
+%
+INC_NONDIM= INITIAL_VALUES
 REF_LENGTH= 1.0
 REF_AREA= 2.0
+%
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
+%
 MARKER_HEATFLUX= ( wall, 0.0 )
+MARKER_SYM= ( symmetry )
+%
 INC_INLET_TYPE= VELOCITY_INLET
 MARKER_INLET= ( inlet, 302.4, 70.0, 1.0, 0.0, 0.0 )
+%
 INC_OUTLET_TYPE= PRESSURE_OUTLET PRESSURE_OUTLET
 MARKER_OUTLET= ( outlet, 0.0, farfield, 0.0 )
-MARKER_SYM= ( symmetry )
-MARKER_PLOTTING= ( wall )
-MARKER_MONITORING= ( wall )
+%
 % ------------------------ WALL FUNCTION DEFINITION --------------------------%
 %
 MARKER_WALL_FUNCTIONS= ( wall, STANDARD_WALL_FUNCTION )
@@ -50,10 +56,12 @@ WALLMODEL_MAXITER= 200
 WALLMODEL_RELFAC= 0.5
 %
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
+%
 NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 1e2
 CFL_ADAPT= NO
 ITER= 1000
+%
 % ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
 %
 LINEAR_SOLVER= FGMRES
@@ -62,22 +70,29 @@ LINEAR_SOLVER_ERROR= 1e-15
 LINEAR_SOLVER_ITER= 10
 %
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
+%
 MGLEVEL= 0
+%
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
+%
 CONV_NUM_METHOD_FLOW= FDS
 MUSCL_FLOW= YES
 SLOPE_LIMITER_FLOW= NONE
 TIME_DISCRE_FLOW= EULER_IMPLICIT
+%
 % -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
+%
 CONV_NUM_METHOD_TURB= SCALAR_UPWIND
 MUSCL_TURB= NO
 SLOPE_LIMITER_TURB= NONE
 TIME_DISCRE_TURB= EULER_IMPLICIT
+%
 % --------------------------- CONVERGENCE PARAMETERS --------------------------%
 CONV_RESIDUAL_MINVAL= -17
 CONV_STARTITER= 10
 CONV_CAUCHY_ELEMS= 100
 CONV_CAUCHY_EPS= 1E-6
+%
 % ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
 %
 MESH_FILENAME= ../mesh_flatplate_140x100.su2
@@ -88,7 +103,9 @@ SCREEN_OUTPUT= (INNER_ITER, WALL_TIME, RMS_PRESSURE, RMS_VELOCITY-X, RMS_VELOCIT
 SCREEN_WRT_FREQ_INNER= 10
 %
 HISTORY_OUTPUT= (ITER, RMS_RES, AERO_COEFF, FLOW_COEFF)
+MARKER_PLOTTING= ( wall )
+MARKER_MONITORING= ( wall )
 %
 OUTPUT_FILES= RESTART, PARAVIEW_MULTIBLOCK
-VOLUME_OUTPUT= RESIDUAL
+VOLUME_OUTPUT= RESIDUAL, PRIMITIVE, RESIDUAL
 OUTPUT_WRT_FREQ= 1000