diff --git a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp b/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp index d53e92e24da4..ca21c93e1dfe 100644 --- a/SU2_CFD/src/numerics/NEMO/NEMO_sources.cpp +++ b/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)); diff --git a/SU2_CFD/src/numerics/flow/flow_sources.cpp b/SU2_CFD/src/numerics/flow/flow_sources.cpp index 49a6e5715ae6..354f5d06f445 100644 --- a/SU2_CFD/src/numerics/flow/flow_sources.cpp +++ b/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])); diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py index 1562b6298598..10c8d98d733b 100644 --- a/TestCases/hybrid_regression.py +++ b/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) ################################# diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py index 2d6eb9772609..dbaab919878d 100644 --- a/TestCases/parallel_regression.py +++ b/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 diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py index c7576f3999e9..7357ab104fd8 100644 --- a/TestCases/serial_regression.py +++ b/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