Add CylinderChandrasekarRoe test case. Residuals to be updated yet

Author: loganoz

.github/workflows/CI_parallel.yml

@@ -136,6 +136,25 @@ jobs:
          make MODE=${{matrix.mode}} COMPILER=${{matrix.compiler}} COMM=${{matrix.comm}} ENABLE_THREADS=${{matrix.enable_threads}} WITH_METIS=YES
 
 
+#
+# 0) CYLINDER ChandrasekarRoe
+# ------------------
+
+      - name: Build NSCylinderChandrasekarRoe
+        working-directory: ./Solver/test/NavierStokes/CylinderChandrasekarRoe/SETUP
+        run: |
+          source /opt/intel/oneapi/setvars.sh || true
+          make MODE=${{matrix.mode}} COMPILER=${{matrix.compiler}} COMM=${{matrix.comm}} ENABLE_THREADS=${{matrix.enable_threads}} WITH_MKL=${{matrix.mkl}} WITH_HDF5=${{matrix.hdf5}}
+        if: '!cancelled()'
+
+      - name: Run NSCylinderChandrasekarRoe
+        working-directory: ./Solver/test/NavierStokes/CylinderChandrasekarRoe
+        run: |
+          source /opt/intel/oneapi/setvars.sh || true
+          mpiexec -n 8 ./horses3d.ns CylinderChandrasekarRoe.control
+        if: '!cancelled()'
+
+
 ########################################################################
 #######                         EULER                           ########
 ########################################################################

.github/workflows/CI_sequential 2.yml

@@ -116,6 +116,25 @@ jobs:
 #######                         NAVIER-STOKES                   ########
 ########################################################################
 
+#
+# 0) CYLINDER ChandrasekarRoe
+# ------------------
+
+      - name: Build NSCylinderChandrasekarRoe
+        working-directory: ./Solver/test/NavierStokes/CylinderChandrasekarRoe/SETUP
+        run: |
+          source /opt/intel/oneapi/setvars.sh || true
+          make MODE=${{matrix.mode}} COMPILER=${{matrix.compiler}} COMM=${{matrix.comm}} ENABLE_THREADS=${{matrix.enable_threads}} WITH_MKL=${{matrix.mkl}} WITH_HDF5=${{matrix.hdf5}}
+        if: '!cancelled()'
+
+      - name: Run NSCylinderChandrasekarRoe
+        working-directory: ./Solver/test/NavierStokes/CylinderChandrasekarRoe
+        run: |
+          source /opt/intel/oneapi/setvars.sh || true
+          ./horses3d.ns CylinderChandrasekarRoe.control
+        if: '!cancelled()'
+
+
 #
 # 0) Convergence
 # ------------------------------

Solver/configure

@@ -55,6 +55,7 @@ TEST_CASES="./Euler/BoxAroundCircle \
             ./NavierStokes/CylinderSmagorinsky \
             ./NavierStokes/CylinderWALE \
             ./NavierStokes/CylinderVreman \
+            ./NavierStokes/CylinderChandrasekarRoe \
             ./NavierStokes/IBM_Cylinder \
             ./NavierStokes/DualTimeStepping \
             ./NavierStokes/EntropyConservingTest \

Solver/test/NavierStokes/CylinderChandrasekarRoe/CylinderChandrasekarRoe.control

@@ -0,0 +1,69 @@
+Flow equations        = "NS"
+mesh file name        = "../../TestMeshes/CylinderNSpol3.mesh"
+Polynomial order      = 3
+Number of time steps  = 100
+Output Interval       = 10
+Number of plot points = 5
+Convergence tolerance = 1.d-10
+cfl                   = 0.3
+dcfl                  = 0.3
+mach number           = 0.3
+Reynolds number       = 200.0
+AOA theta             = 0.0
+AOA phi               = 90.0
+solution file name    = "RESULTS/Cylinder.hsol"
+save gradients with solution = .true.
+restart               = .false.
+restart file name     = "RESULTS/Cylinder.hsol"
+riemann solver          = Roe
+Discretization nodes    = Gauss-Lobatto
+inviscid discretization = Split-Form
+averaging               = Chandrasekar
+Viscous discretization  = BR1
+
+#define boundary InnerCylinder
+      type = NoSlipWall
+#end
+
+#define boundary Front__Back__Left
+      type = Inflow
+#end
+
+#define boundary Bottom__Top
+      type = FreeSlipWall
+#end
+
+#define boundary Right
+      type = Outflow
+#end
+
+
+#define surface monitor 1
+   Name = cyl-drag
+   Marker = innercylinder
+   Variable = drag
+   Direction = [0.0,0.0,1.0]
+   Reference surface = 1.0	
+#end
+
+#define surface monitor 2
+   Name = cyl-lift
+   Marker = innercylinder
+   Variable = lift
+   Direction = [1.0,0.0,0.0]
+   Reference surface = 1.0
+#end
+
+#define probe 1
+   Name = wake_u
+   Position = [0.0,2.0,4.0]
+   Variable = u
+#end
+
+!#define statistics
+!   Sampling interval = 10
+!   Starting iteration = 15
+!   Starting time = 0.0
+!   @start*
+!   @stop
+!#end