fix some version numbers

Author: pcarruscag

.github/workflows/change-version.yml

@@ -16,7 +16,7 @@ jobs:
       id: extract_branch
     - name: Change the version number
       run: |
-        SU2_PY/change_version_number.py -v ${GITHUB_REF##*/release_v} -r Blackbird -y
+        SU2_PY/change_version_number.py -v ${GITHUB_REF##*/release_v} -r Harrier -y
     - name: Commit files
       run: |
         git config --local user.email "action@github.com"

TestCases/flamelet/05_laminar_premixed_ch4_flame_cfd_axi/lam_prem_ch4_cfd_axi.cfg

@@ -1,11 +1,11 @@
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 % SU2 configuration file                                                       %
 % Case description: Laminar premixed flame stabilized on isothermal burner     %
-%                   axisymmetric setup
+%                   axisymmetric setup                                         %
 % Author: Nijso Beishuizen                                                     %
 % Institution: Bosch Thermotechnology                                          %
 % Date: 08/09/2021                                                             %
-% File Version 7.5.0 "Falcon", branch: feature_new_flamelet                    %
+% File Version 7.5.1 "Blackbird",                                              %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 %
@@ -25,7 +25,7 @@ INC_VELOCITY_INIT= (0.5, 0.0, 0.0 )
 INC_TEMPERATURE_INIT= 300.0
 INC_NONDIM= DIMENSIONAL
 %
-% 
+%
 AXISYMMETRIC= YES
 % -------------------- FLUID MODEL --------------------------------------- %
 %
@@ -36,7 +36,7 @@ CONTROLLING_VARIABLE_SOURCE_NAMES= (ProdRateTot_PV, NULL)
 %
 % -------------------- SCALAR TRANSPORT ---------------------------------------%
 %
-KIND_SCALAR_MODEL= FLAMELET      
+KIND_SCALAR_MODEL= FLAMELET
 DIFFUSIVITY_MODEL= FLAMELET
 VISCOSITY_MODEL= FLAMELET
 CONDUCTIVITY_MODEL= FLAMELET
@@ -127,12 +127,12 @@ MESH_FILENAME= mesh_axi.su2
 MESH_OUT_FILENAME= mesh_out.su2
 SOLUTION_FILENAME= solution
 RESTART_FILENAME= restart
-%OUTPUT_FILES= (RESTART,PARAVIEW,PARAVIEW_MULTIBLOCK) 
-OUTPUT_FILES= (RESTART) 
+%OUTPUT_FILES= (RESTART,PARAVIEW,PARAVIEW_MULTIBLOCK)
+OUTPUT_FILES= (RESTART)
 TABULAR_FORMAT= CSV
 CONV_FILENAME= history
 VOLUME_FILENAME= flow
 SURFACE_FILENAME= surface_flow
-WRT_PERFORMANCE= NO 
+WRT_PERFORMANCE= NO
 SCREEN_WRT_FREQ_INNER= 1
 SCREEN_WRT_FREQ_OUTER= 1

TestCases/nicf/datadriven/datadriven_nozzle.cfg

@@ -7,7 +7,7 @@
 % Author: Evert Bunschoten                                                     %
 % Institution: Delft University of Technology                                  %
 % Date: 2022.10.8                                                              %
-% File Version  7.4.0 Blackbird                                                %
+% File Version  7.5.1 Blackbird                                                %
 %                                                                              %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -36,7 +36,7 @@ REF_DIMENSIONALIZATION= DIMENSIONAL
 % ---- DATADRIVEN FLUID MODEL DEFINITION -------%
 %
 FLUID_MODEL = DATADRIVEN_FLUID
-INTERPOLATION_METHOD = MLP 
+INTERPOLATION_METHOD = MLP
 FILENAMES_INTERPOLATOR = (MLP_air.mlp)
 DATADRIVEN_NEWTON_RELAXATION = 0.8
 

TestCases/vandv/species_transport/sandia_jet/validation.cfg

@@ -5,7 +5,7 @@
 % Author: S.J.H. Bosmans                                                            %
 % Institution: TU Eindhoven (TU/e)                                                  %
 % Date: 2023/05/04                                                                  %
-% File Version 7.5.0 "Blackbird"                                                    %
+% File Version 7.5.1 "Blackbird"                                                    %
 %                                                                                   %
 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
@@ -48,8 +48,8 @@ PRANDTL_TURB= 0.90, 0.90
 %
 VISCOSITY_MODEL= CONSTANT_VISCOSITY
 %
-MU_CONSTANT= 8.04E-06, 1.8551E-05 
-% 
+MU_CONSTANT= 8.04E-06, 1.8551E-05
+%
 MIXING_VISCOSITY_MODEL = WILKE
 %
 % -------------------- BOUNDARY CONDITION DEFINITION --------------------------%