Merge pull request #1366 from su2code/fix_axisym

fix bug axisym source term + update regression cases

Author: FlorianDm

SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp

@@ -378,7 +378,7 @@ CNumerics::ResidualType<> CSource_NEMO::ComputeAxisymmetric(const CConfig *confi
     residual[nSpecies+1] -= Volume*(yinv*total_viscosity_i*2*(GV[nSpecies+3][1]-v*yinv)
                                                              -TWO3*AuxVar_Grad_i[0][1]);
     residual[nSpecies+2] -= Volume*(yinv*(-sumJhs_y + total_viscosity_i*(u*(GV[nSpecies+3][0]+GV[nSpecies+2][1])
-                                                                        +v*TWO3*(2*GV[nSpecies+2][1]-GV[nSpecies+2][0]
+                                                                        +v*TWO3*(2*GV[nSpecies+3][1]-GV[nSpecies+2][0]
                                                                         -v*yinv+rho*turb_ke_i))-qy_t)
                                                                         -TWO3*(AuxVar_Grad_i[1][1]+AuxVar_Grad_i[2][0]));
     residual[nSpecies+3] -= Volume*(yinv*(-sumJeve_y -qy_ve));

SU2_CFD/src/numerics/flow/flow_sources.cpp

@@ -154,7 +154,7 @@ void CSourceAxisymmetric_Flow::ResidualDiffusion(){
   residual[2] -= Volume*(yinv*total_viscosity_i*2*(PrimVar_Grad_i[2][1]-v*yinv)
                          -TWO3*AuxVar_Grad_i[0][1]);
   residual[3] -= Volume*(yinv*(total_viscosity_i*(u*(PrimVar_Grad_i[2][0]+PrimVar_Grad_i[1][1])
-                                                 +v*TWO3*(2*PrimVar_Grad_i[1][1]-PrimVar_Grad_i[1][0]
+                                                 +v*TWO3*(2*PrimVar_Grad_i[2][1]-PrimVar_Grad_i[1][0]
                                                  -v*yinv+U_i[0]*turb_ke_i))
                                                  +total_conductivity_i*PrimVar_Grad_i[0][1])
                                                  -TWO3*(AuxVar_Grad_i[1][1]+AuxVar_Grad_i[2][0]));

TestCases/hybrid_regression.py

@@ -227,7 +227,7 @@ def main():
     axi_rans_air_nozzle.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle.cfg_file  = "air_nozzle.cfg"
     axi_rans_air_nozzle.test_iter = 10
-    axi_rans_air_nozzle.test_vals = [-6.348077, -0.827162, -2.241982, 2.313210]
+    axi_rans_air_nozzle.test_vals = [-12.094009, -6.643017, -8.900656, -2.393294]
     test_list.append(axi_rans_air_nozzle)
 
     #################################

TestCases/parallel_regression.py

@@ -83,7 +83,7 @@ def main():
     visc_cone.cfg_dir   = "nonequilibrium/axi_visccone"
     visc_cone.cfg_file  = "axi_visccone.cfg"
     visc_cone.test_iter = 10
-    visc_cone.test_vals = [-5.173082, -5.697844, -20.831292, -20.719160, -23.419769, -1.564064, -2.069008, 2.203919, -2.590729]
+    visc_cone.test_vals = [-5.173078, -5.697841, -20.831296, -20.719164, -23.419769, -1.564084, -2.069040, 2.203924, -2.590729]
     visc_cone.su2_exec  = "mpirun -n 2 SU2_CFD"
     visc_cone.timeout   = 1600
     visc_cone.new_output = True
@@ -389,7 +389,7 @@ def main():
     axi_rans_air_nozzle.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle.cfg_file  = "air_nozzle.cfg"
     axi_rans_air_nozzle.test_iter = 10
-    axi_rans_air_nozzle.test_vals = [-6.278454, -0.744813, -2.243285, 2.312481]
+    axi_rans_air_nozzle.test_vals = [-12.098340, -6.651791, -8.877009, -2.393286]
     axi_rans_air_nozzle.su2_exec  = "mpirun -n 2 SU2_CFD"
     axi_rans_air_nozzle.timeout   = 1600
     axi_rans_air_nozzle.tol       = 0.0001

TestCases/serial_regression.py

@@ -81,7 +81,7 @@ def main():
     visc_cone.cfg_dir   = "nonequilibrium/axi_visccone"
     visc_cone.cfg_file  = "axi_visccone.cfg"
     visc_cone.test_iter = 10
-    visc_cone.test_vals = [-5.173082, -5.697844, -20.831292, -20.719160, -23.419769, -1.564064, -2.069008, 2.203919, -2.590729]
+    visc_cone.test_vals = [-5.173078, -5.697841, -20.831296, -20.719164, -23.419769, -1.564084, -2.069040, 2.203924, -2.590729]
     visc_cone.su2_exec  = "SU2_CFD"
     visc_cone.timeout   = 1600
     visc_cone.new_output = True
@@ -395,7 +395,7 @@ def main():
     axi_rans_air_nozzle.cfg_dir   = "axisymmetric_rans/air_nozzle"
     axi_rans_air_nozzle.cfg_file  = "air_nozzle.cfg"
     axi_rans_air_nozzle.test_iter = 10
-    axi_rans_air_nozzle.test_vals = [ -6.279299, -0.747627, -2.237638, 2.321596]
+    axi_rans_air_nozzle.test_vals = [-12.097563, -6.650115, -8.875944, -2.393285]
     axi_rans_air_nozzle.su2_exec  = "SU2_CFD"
     axi_rans_air_nozzle.timeout   = 1600
     axi_rans_air_nozzle.tol       = 0.0001