updated Aachen config and regression test

Author: alecappiello

.github/workflows/regression.yml

@@ -209,7 +209,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2:240320-1536
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}}
+          args: -b ${{github.ref}} -t develop -c fix_aachen_testcase -s ${{matrix.testscript}}
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2:240320-1536
         with:
@@ -255,7 +255,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2-tsan:240320-1536
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}} -a "--tsan"
+          args: -b ${{github.ref}} -t develop -c fix_aachen_testcase -s ${{matrix.testscript}} -a "--tsan"
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2-tsan:240320-1536
         with:
@@ -300,7 +300,7 @@ jobs:
         uses: docker://ghcr.io/su2code/su2/test-su2-asan:240320-1536
         with:
           # -t <Tutorials-branch> -c <Testcases-branch>
-          args: -b ${{github.ref}} -t develop -c develop -s ${{matrix.testscript}} -a "--asan"
+          args: -b ${{github.ref}} -t develop -c fix_aachen_testcase -s ${{matrix.testscript}} -a "--asan"
       - name: Cleanup
         uses: docker://ghcr.io/su2code/su2/test-su2-asan:240320-1536
         with:

TestCases/turbomachinery/Aachen_turbine/aachen_3D_MP_restart.cfg

@@ -119,6 +119,15 @@ CONDUCTIVITY_MODEL= CONSTANT_PRANDTL
 %Navier-Stokes wall boundary marker(s) (NONE = no marker)
 MARKER_HEATFLUX= (BLADE1, 0.0, BLADE2, 0.0, BLADE3, 0.0, HUB1, 0.0, SHROUD1, 0.0, HUB2, 0.0, SHROUD2, 0.0, HUB3, 0.0, SHROUD3, 0.0)
 %
+% ------------------------ WALL FUNCTION DEFINITION --------------------------%
+%
+MARKER_WALL_FUNCTIONS= ( BLADE1, STANDARD_WALL_FUNCTION , BLADE2, STANDARD_WALL_FUNCTION , BLADE3, STANDARD_WALL_FUNCTION , HUB1, STANDARD_WALL_FUNCTION , SHROUD1, STANDARD_WALL_FUNCTION , HUB2, STANDARD_WALL_FUNCTION , SHROUD2, STANDARD_WALL_FUNCTION , HUB3, STANDARD_WALL_FUNCTION , SHROUD3, STANDARD_WALL_FUNCTION )
+WALLMODEL_KAPPA= 0.41
+WALLMODEL_B= 5.5
+WALLMODEL_MINYPLUS= 5.0
+WALLMODEL_MAXITER= 200
+WALLMODEL_RELFAC= 0.5
+
 % Periodic boundary marker(s) (NONE = no marker)
 % Format: ( periodic marker, donor marker, rot_cen_x, rot_cen_y, rot_cen_z, rot_angle_x-axis, rot_angle_y-axis, rot_angle_z-axis, translation_x, translation_y, translation_z)
 MARKER_PERIODIC= (PER1_STATOR1, PER2_STATOR1, 0.0, 0.0, 0.0, 0.0, 0.0, 8.7804878, 0.0, 0.0, 0.0, PER1_ROTOR, PER2_ROTOR, 0.0, 0.0, 0.0, 0.0, 0.0, 8.7804878, 0.0, 0.0, 0.0, PER1_STATOR2, PER2_STATOR2, 0.0, 0.0, 0.0, 0.0, 0.0, 8.7804878, 0.0, 0.0, 0.0)
@@ -164,10 +173,10 @@ MIXINGPLANE_INTERFACE_KIND= LINEAR_INTERPOLATION
 TURBULENT_MIXINGPLANE= YES
 %
 % Specify ramp option for Outlet pressure (YES, NO) default NO
-RAMP_OUTLET_PRESSURE= NO
+RAMP_OUTLET_PRESSURE= YES
 %
 % Parameters of the outlet pressure ramp (starting outlet pressure, updating-iteration-frequency, total number of iteration for the ramp)
-RAMP_OUTLET_PRESSURE_COEFF= (140000.0, 10.0, 2000)
+RAMP_OUTLET_PRESSURE_COEFF= (140000.0, 150.0, 2000)
 %
 % Specify Kind of average process for linearizing the Navier-Stokes equation at inflow and outflow BC included mixing-plane
 % (ALGEBRAIC, AREA, MASSSFLUX, MIXEDOUT) default AREA 
@@ -196,7 +205,7 @@ MARKER_MONITORING= (BLADE1, BLADE2, BLADE3)
 NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
 %
 % Courant-Friedrichs-Lewy condition of the finest grid
-CFL_NUMBER= 10
+CFL_NUMBER= 2
 %
 % Adaptive CFL number (NO, YES)
 CFL_ADAPT= NO
@@ -230,8 +239,8 @@ LIMITER_ITER= 999999
 % -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
 %
 % Convective numerical method 
-CONV_NUM_METHOD_FLOW= ROE
-ENTROPY_FIX_COEFF= 0.001
+CONV_NUM_METHOD_FLOW= JST
+ENTROPY_FIX_COEFF= 0.3
 %
 JST_SENSOR_COEFF= ( 0.5, 0.25 )
 % Spatial numerical order integration 
@@ -294,7 +303,7 @@ CONV_RESIDUAL_MINVAL= -12
 CONV_STARTITER= 10
 %
 % Screen output fields (use 'SU2_CFD -d <config_file>' to view list of available fields)
-SCREEN_OUTPUT= (OUTER_ITER, RMS_DENSITY[0], RMS_DENSITY[1], RMS_DENSITY[2], RMS_MOMENTUM-X[0], RMS_MOMENTUM-Y[0], RMS_ENERGY[0])
+SCREEN_OUTPUT= (OUTER_ITER, RMS_DENSITY[0], RMS_DENSITY[1], RMS_DENSITY[2], RMS_MOMENTUM-X[0], RMS_MOMENTUM-X[1], RMS_MOMENTUM-X[2], RMS_MOMENTUM-Y[0], RMS_MOMENTUM-Y[1], RMS_MOMENTUM-Y[2], RMS_MOMENTUM-Z[0], RMS_MOMENTUM-Z[1], RMS_MOMENTUM-Z[2], RMS_ENERGY[0], RMS_ENERGY[1], RMS_ENERGY[2])
 %
 % History output groups (use 'SU2_CFD -d <config_file>' to view list of available fields)
 HISTORY_OUTPUT= (ITER, RMS_RES, TURBO_PERF)
@@ -349,7 +358,7 @@ SURFACE_FILENAME= surface_flow
 SURFACE_ADJ_FILENAME= surface_adjoint
 %
 % Writing solution file frequency
-OUTPUT_WRT_FREQ= 500
+OUTPUT_WRT_FREQ= 1000
 %
 % Writing convergence history frequency
 HISTORY_WRT_FREQ_OUTER= 1