diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp
index 32c265e55656..b1c61ad377de 100644
--- a/SU2_CFD/src/solvers/CEulerSolver.cpp
+++ b/SU2_CFD/src/solvers/CEulerSolver.cpp
@@ -2551,9 +2551,13 @@ void CEulerSolver::ComputeUnderRelaxationFactor(const CConfig* config) {
su2double ratio = fabs(LinSysSol(iPoint, 0)) / max(nodes->GetSolution(iPoint, 0), EPS);
su2double e_old = nodes->GetSolution(iPoint, nVar - 1);
su2double e_new = e_old + LinSysSol(iPoint, nVar - 1);
- for (unsigned short jVar = 1; jVar <= nDim; jVar++) {
- e_old -= 0.5 * pow(nodes->GetSolution(iPoint, jVar), 2);
- e_new -= 0.5 * pow(nodes->GetSolution(iPoint, jVar) + LinSysSol(iPoint, jVar), 2);
+ /*--- rho*e = rho*E - |rho*u|^2 / (2*rho), with the old and the proposed new density. ---*/
+ /*--- Materialize CoDi expressions: GetSolution returns temporary active scalars. ---*/
+ const su2double rho_old = max(nodes->GetSolution(iPoint, 0), EPS);
+ const su2double rho_new = max(rho_old + LinSysSol(iPoint, 0), EPS);
+ for (auto jVar = 1u; jVar <= nDim; jVar++) {
+ e_old -= 0.5 * pow(nodes->GetSolution(iPoint, jVar), 2) / rho_old;
+ e_new -= 0.5 * pow(nodes->GetSolution(iPoint, jVar) + LinSysSol(iPoint, jVar), 2) / rho_new;
}
ratio = fmax(ratio, fabs(e_new - e_old) / max(e_old, EPS));
diff --git a/TestCases/cont_adj_euler/naca0012/of_grad_directdiff.dat.ref b/TestCases/cont_adj_euler/naca0012/of_grad_directdiff.dat.ref
index c87c1c9a2a49..2e6cd4903a0d 100644
--- a/TestCases/cont_adj_euler/naca0012/of_grad_directdiff.dat.ref
+++ b/TestCases/cont_adj_euler/naca0012/of_grad_directdiff.dat.ref
@@ -1,4 +1,4 @@
VARIABLES="VARIABLE" , "DRAG" , "EFFICIENCY" , "FORCE_X" , "FORCE_Y" , "FORCE_Z" , "LIFT" , "MOMENT_X" , "MOMENT_Y" , "MOMENT_Z" , "SIDEFORCE"
- 0 , -0.4704786435 , -33.40446141 , -0.3888715474 , -3.745132593 , 0.0 , -3.735758164 , 0.0 , 0.0 , 0.4834798526 , 0.0
- 1 , 0.412031843 , -39.78218403 , 0.4880368175 , -3.47876392 , 0.0 , -3.488582535 , 0.0 , 0.0 , 0.2021305183 , 0.0
- 2 , 0.8908446367 , -37.475187 , 0.9514902759 , -2.769632304 , 0.0 , -2.789729858 , 0.0 , 0.0 , -0.1182204408 , 0.0
+ 0 , -0.4834688689 , -33.38043366 , -0.4014654728 , -3.763436475 , 0.0 , -3.753782956 , 0.0 , 0.0 , 0.4865376034 , 0.0
+ 1 , 0.4087842111 , -39.69099805 , 0.4848740806 , -3.482690031 , 0.0 , -3.492438718 , 0.0 , 0.0 , 0.2039858924 , 0.0
+ 2 , 0.8921290437 , -37.32658951 , 0.9526325615 , -2.763104959 , 0.0 , -2.783228985 , 0.0 , 0.0 , -0.117214663 , 0.0
diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py
index f63748ba9283..4102f44efa42 100644
--- a/TestCases/hybrid_regression.py
+++ b/TestCases/hybrid_regression.py
@@ -72,7 +72,7 @@ def main():
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 20
- naca0012.test_vals = [-4.031227, -3.524077, 0.272155, 0.009374]
+ naca0012.test_vals = [-4.029205, -3.521852, 0.272095, 0.009425]
test_list.append(naca0012)
# Supersonic wedge
@@ -80,7 +80,7 @@ def main():
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 20
- wedge.test_vals = [-0.480786, 5.329367, -0.244869, 0.043126]
+ wedge.test_vals = [-4.223565, 1.506875, -0.249526, 0.043953]
test_list.append(wedge)
# ONERA M6 Wing
@@ -104,7 +104,7 @@ def main():
bluntbody.cfg_dir = "euler/bluntbody"
bluntbody.cfg_file = "blunt.cfg"
bluntbody.test_iter = 20
- bluntbody.test_vals = [0.666182, 7.055173, -0.000631, 3.917770]
+ bluntbody.test_vals = [0.565173, 6.945846, 0.000171, 1.970669]
test_list.append(bluntbody)
##########################
@@ -170,7 +170,7 @@ def main():
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 20
- rae2822_sa.test_vals = [-2.639525, -4.027096, 0.792680, 0.020549, 1000.000000]
+ rae2822_sa.test_vals = [-2.858565, -4.906734, 0.782692, 0.018639, 1000.000000]
test_list.append(rae2822_sa)
# RAE2822 SST
@@ -178,7 +178,7 @@ def main():
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 20
- rae2822_sst.test_vals = [-1.501958, 5.889330, 0.635453, 0.021771, 100.000000]
+ rae2822_sst.test_vals = [-1.461774, 5.883885, 0.630267, 0.020404, 100.000000]
test_list.append(rae2822_sst)
# RAE2822 SST_SUST
@@ -202,7 +202,7 @@ def main():
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
- turb_oneram6.test_vals = [-2.418707, -6.631575, 0.238586, 0.159599, 0.000000]
+ turb_oneram6.test_vals = [-2.419971, -6.631992, 0.238576, 0.159694, 0.000000]
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
@@ -265,7 +265,7 @@ def main():
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
axi_rans_air_nozzle_restart.cfg_file = "air_nozzle_restart.cfg"
axi_rans_air_nozzle_restart.test_iter = 10
- axi_rans_air_nozzle_restart.test_vals = [-2.663059, 2.911787, -2.522191, 1.990732, 0.000000]
+ axi_rans_air_nozzle_restart.test_vals = [-5.068875, 0.504406, -2.840213, 1.705449, 0.000000]
axi_rans_air_nozzle_restart.test_vals_aarch64 = [-14.140441, -9.154674, -10.886121, -5.806594, 0.000000]
test_list.append(axi_rans_air_nozzle_restart)
@@ -348,7 +348,7 @@ def main():
hb_rans_preconditioning.cfg_dir = "harmonic_balance/hb_rans_preconditioning"
hb_rans_preconditioning.cfg_file = "davis.cfg"
hb_rans_preconditioning.test_iter = 25
- hb_rans_preconditioning.test_vals = [-1.905220, 0.481910, 0.598990, 3.605349, -5.945852]
+ hb_rans_preconditioning.test_vals = [-1.905523, 0.482128, 0.598472, 3.605108, -5.946081]
test_list.append(hb_rans_preconditioning)
#############################
@@ -581,7 +581,7 @@ def main():
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 25
- edge_VW.test_vals = [-11.670757, -5.483973, -0.000009, 0.000000]
+ edge_VW.test_vals = [-11.723086, -5.536517, -0.000009, 0.000000]
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
@@ -589,7 +589,7 @@ def main():
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 20
- edge_PPR.test_vals = [-12.338051, -6.157966, -0.000034, 0.000000]
+ edge_PPR.test_vals = [-10.993286, -4.827527, -0.000034, 0.000000]
edge_PPR.test_vals_aarch64 = [ -7.139211, -0.980821, -0.000034, 0.000000]
test_list.append(edge_PPR)
@@ -659,7 +659,7 @@ def main():
channel_2D.cfg_dir = "sliding_interface/channel_2D"
channel_2D.cfg_file = "channel_2D_WA.cfg"
channel_2D.test_iter = 2
- channel_2D.test_vals = [2.000000, 0.000000, 0.466194, 0.350087, 0.398979]
+ channel_2D.test_vals = [2.000000, 0.000000, 0.466339, 0.346858, 0.397486]
channel_2D.unsteady = True
channel_2D.multizone = True
test_list.append(channel_2D)
@@ -669,7 +669,7 @@ def main():
channel_3D.cfg_dir = "sliding_interface/channel_3D"
channel_3D.cfg_file = "channel_3D_WA.cfg"
channel_3D.test_iter = 2
- channel_3D.test_vals = [2.000000, 0.000000, 0.632251, 0.534213, 0.431803]
+ channel_3D.test_vals = [2.000000, 0.000000, 0.632749, 0.522745, 0.423269]
channel_3D.test_vals_aarch64 = [2.000000, 0.000000, 0.629112, 0.524948, 0.422396]
channel_3D.unsteady = True
channel_3D.multizone = True
@@ -681,7 +681,7 @@ def main():
pipe.cfg_dir = "sliding_interface/pipe"
pipe.cfg_file = "pipe_NN.cfg"
pipe.test_iter = 2
- pipe.test_vals = [0.092415, 0.568971, 0.692864, 0.989451, 1.048245]
+ pipe.test_vals = [0.070225, 0.528891, 0.684177, 0.970350, 1.065268]
pipe.unsteady = True
pipe.multizone = True
test_list.append(pipe)
@@ -691,7 +691,7 @@ def main():
rotating_cylinders.cfg_dir = "sliding_interface/rotating_cylinders"
rotating_cylinders.cfg_file = "rot_cylinders_WA.cfg"
rotating_cylinders.test_iter = 3
- rotating_cylinders.test_vals = [3.000000, 0.000000, 0.664817, 1.125803, 1.117608]
+ rotating_cylinders.test_vals = [3.000000, 0.000000, 0.686432, 1.159463, 1.151135]
rotating_cylinders.unsteady = True
rotating_cylinders.multizone = True
test_list.append(rotating_cylinders)
@@ -701,7 +701,7 @@ def main():
supersonic_vortex_shedding.cfg_dir = "sliding_interface/supersonic_vortex_shedding"
supersonic_vortex_shedding.cfg_file = "sup_vor_shed_WA.cfg"
supersonic_vortex_shedding.test_iter = 5
- supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 0.899645, 1.076181]
+ supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.126036, 1.081765]
supersonic_vortex_shedding.unsteady = True
supersonic_vortex_shedding.multizone = True
test_list.append(supersonic_vortex_shedding)
diff --git a/TestCases/multiple_ffd/naca0012/of_grad_cd.dat.ref b/TestCases/multiple_ffd/naca0012/of_grad_cd.dat.ref
index 2f2e345e4221..e98387350993 100644
--- a/TestCases/multiple_ffd/naca0012/of_grad_cd.dat.ref
+++ b/TestCases/multiple_ffd/naca0012/of_grad_cd.dat.ref
@@ -1,3 +1,3 @@
VARIABLES="VARIABLE" , "GRADIENT" , "FINDIFF_STEP"
- 0 , 0.0440381 , 0.001
- 1 , -0.0848429 , 0.001
+ 0 , 0.0439624 , 0.001
+ 1 , -0.0848386 , 0.001
diff --git a/TestCases/multiple_ffd/naca0012/of_grad_directdiff.dat.ref b/TestCases/multiple_ffd/naca0012/of_grad_directdiff.dat.ref
index ef3b2d9f463a..dfad81314570 100644
--- a/TestCases/multiple_ffd/naca0012/of_grad_directdiff.dat.ref
+++ b/TestCases/multiple_ffd/naca0012/of_grad_directdiff.dat.ref
@@ -1,3 +1,3 @@
VARIABLES="VARIABLE" , "DRAG" , "EFFICIENCY" , "FORCE_X" , "FORCE_Y" , "FORCE_Z" , "LIFT" , "MOMENT_X" , "MOMENT_Y" , "MOMENT_Z" , "SIDEFORCE"
- 0 , 0.04790586765 , -0.4797536912 , 0.04825151062 , -0.01531800012 , 0.0 , -0.01636695601 , 0.0 , 0.0 , 0.03036927931 , 0.0
- 1 , -0.09320474204 , 0.3762440542 , -0.0926027588 , -0.02860524743 , 0.0 , -0.02657832162 , 0.0 , 0.0 , 0.06626460628 , 0.0
+ 0 , 0.04764411115 , -0.463384101 , 0.04796070834 , -0.01398970686 , 0.0 , -0.01503263502 , 0.0 , 0.0 , 0.03019600866 , 0.0
+ 1 , -0.09347608871 , 0.3646170468 , -0.0928475452 , -0.02982544755 , 0.0 , -0.02779289138 , 0.0 , 0.0 , 0.06643204278 , 0.0
diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py
index e79219efbeba..1a6560f90f34 100755
--- a/TestCases/parallel_regression.py
+++ b/TestCases/parallel_regression.py
@@ -266,7 +266,7 @@ def main():
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe_su2bin.cfg"
naca0012.test_iter = 20
- naca0012.test_vals = [-4.026356, -3.521920, 0.274929, 0.009852]
+ naca0012.test_vals = [-4.024996, -3.520626, 0.275033, 0.009889]
test_list.append(naca0012)
# Supersonic wedge
@@ -274,7 +274,7 @@ def main():
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 20
- wedge.test_vals = [-4.142624, 1.585638, -0.249527, 0.043953]
+ wedge.test_vals = [-4.018855, 1.708167, -0.249527, 0.043953]
test_list.append(wedge)
# ONERA M6 Wing
@@ -300,7 +300,7 @@ def main():
polar_naca0012.cfg_file = "inv_NACA0012.cfg"
polar_naca0012.polar = True
polar_naca0012.test_iter = 10
- polar_naca0012.test_vals = [-1.315764, 4.158361, 0.002646, 0.114559]
+ polar_naca0012.test_vals = [-1.315882, 4.158313, 0.002698, 0.114644]
polar_naca0012.test_vals_aarch64 = [-1.083394, 4.386134, 0.001588, 0.033513]
polar_naca0012.command = TestCase.Command(exec = "compute_polar.py", param = "-i 11")
# flaky test on arm64
@@ -312,7 +312,7 @@ def main():
bluntbody.cfg_dir = "euler/bluntbody"
bluntbody.cfg_file = "blunt.cfg"
bluntbody.test_iter = 20
- bluntbody.test_vals = [0.666133, 7.054751, -0.000051, 3.912894]
+ bluntbody.test_vals = [0.565207, 6.945909, -0.000001, 1.970304]
test_list.append(bluntbody)
# Equivalent area NACA64-206
@@ -320,7 +320,7 @@ def main():
ea_naca64206.cfg_dir = "optimization_euler/equivalentarea_naca64206"
ea_naca64206.cfg_file = "NACA64206.cfg"
ea_naca64206.test_iter = 10
- ea_naca64206.test_vals = [-1.125734, -0.473873, -0.002416, 67775.000000]
+ ea_naca64206.test_vals = [-1.126282, -0.474499, -0.002405, 67775.000000]
test_list.append(ea_naca64206)
# SUPERSONIC FLOW PAST A RAMP IN A CHANNEL
@@ -345,7 +345,7 @@ def main():
MFR_coupling.cfg_dir = "euler/turbofan_MFR_coupling"
MFR_coupling.cfg_file = "MFR_coupling.cfg"
MFR_coupling.test_iter = 100
- MFR_coupling.test_vals = [-211.240000, 150.030000, 20.151000]
+ MFR_coupling.test_vals = [-211.250000, 150.030000, 20.151000]
test_list.append(MFR_coupling)
##########################
@@ -390,7 +390,7 @@ def main():
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
- cylinder.test_vals = [-8.557685, -3.072812, -0.018904, 1.610320, 0.000000]
+ cylinder.test_vals = [-8.557718, -3.072847, -0.018912, 1.610317, 0.000000]
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
@@ -430,7 +430,7 @@ def main():
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 20
- rae2822_sa.test_vals = [-2.888183, -5.136146, 0.788144, 0.019032, 1000.000000]
+ rae2822_sa.test_vals = [-2.998634, -4.043296, 0.794248, 0.019260, 1000.000000]
test_list.append(rae2822_sa)
# RAE2822 SST
@@ -438,7 +438,7 @@ def main():
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 20
- rae2822_sst.test_vals = [-1.495621, 5.875629, 0.638353, 0.020410, 100.000000]
+ rae2822_sst.test_vals = [-1.485957, 5.891491, 0.675200, 0.023427, 100.000000]
test_list.append(rae2822_sst)
# RAE2822 SST_SUST
@@ -470,7 +470,7 @@ def main():
turb_flatplate_CC_Wilcox.cfg_dir = "rans/flatplate"
turb_flatplate_CC_Wilcox.cfg_file = "turb_SST_flatplate_compressibility_Wilcox.cfg"
turb_flatplate_CC_Wilcox.test_iter = 20
- turb_flatplate_CC_Wilcox.test_vals = [-1.169750, 2.167973, 1.488567, 5.244807, -3.795767, 9.699598]
+ turb_flatplate_CC_Wilcox.test_vals = [-1.204997, 2.149390, 1.396996, 5.216302, -3.821981, 9.707535]
test_list.append(turb_flatplate_CC_Wilcox)
# Flat plate SST compressibility correction Sarkar
@@ -478,7 +478,7 @@ def main():
turb_flatplate_CC_Sarkar.cfg_dir = "rans/flatplate"
turb_flatplate_CC_Sarkar.cfg_file = "turb_SST_flatplate_compressibility_Sarkar.cfg"
turb_flatplate_CC_Sarkar.test_iter = 20
- turb_flatplate_CC_Sarkar.test_vals = [-1.169750, 2.167973, 1.488567, 5.244807, -3.795765, 9.699598]
+ turb_flatplate_CC_Sarkar.test_vals = [-1.204997, 2.149390, 1.396996, 5.216302, -3.821978, 9.707535]
test_list.append(turb_flatplate_CC_Sarkar)
# FLAT PLATE, ROUGHNESS BC KNOPP SST
@@ -510,7 +510,7 @@ def main():
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
- turb_oneram6.test_vals = [-2.418711, -6.631576, 0.238587, 0.159599, 0.000000]
+ turb_oneram6.test_vals = [-2.419976, -6.631992, 0.238577, 0.159694, 0.000000]
turb_oneram6.timeout = 3200
test_list.append(turb_oneram6)
@@ -519,7 +519,7 @@ def main():
turb_oneram6_vc.cfg_dir = "rans/oneram6"
turb_oneram6_vc.cfg_file = "turb_ONERAM6_vc.cfg"
turb_oneram6_vc.test_iter = 15
- turb_oneram6_vc.test_vals = [-2.294311, -6.572307, 0.234416, 0.144830, 0.000000]
+ turb_oneram6_vc.test_vals = [-2.295077, -6.572734, 0.234428, 0.145063, 0.000000]
turb_oneram6_vc.timeout = 3200
test_list.append(turb_oneram6_vc)
@@ -528,7 +528,7 @@ def main():
turb_oneram6_nk.cfg_dir = "rans/oneram6"
turb_oneram6_nk.cfg_file = "turb_ONERAM6_nk.cfg"
turb_oneram6_nk.test_iter = 20
- turb_oneram6_nk.test_vals = [-4.848809, -4.451213, -11.426556, 0.221554, 0.049197, 2.000000, -0.880072, 10.000000]
+ turb_oneram6_nk.test_vals = [-4.848121, -4.450658, -11.426212, 0.221522, 0.049358, 2.000000, -0.879182, 10.000000]
turb_oneram6_nk.timeout = 600
turb_oneram6_nk.tol = 0.0001
test_list.append(turb_oneram6_nk)
@@ -627,7 +627,7 @@ def main():
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
axi_rans_air_nozzle_restart.cfg_file = "air_nozzle_restart.cfg"
axi_rans_air_nozzle_restart.test_iter = 10
- axi_rans_air_nozzle_restart.test_vals = [-2.662880, 2.912015, -2.712454, 1.890642, 0.000000]
+ axi_rans_air_nozzle_restart.test_vals = [-5.144760, 0.426779, -2.900513, 1.606061, 0.000000]
axi_rans_air_nozzle_restart.test_vals_aarch64 = [-14.143310, -9.163287, -10.858232, -5.787715, 0.000000]
axi_rans_air_nozzle_restart.tol = 0.0001
test_list.append(axi_rans_air_nozzle_restart)
@@ -891,7 +891,7 @@ def main():
turbmod_sa_bsl_rae2822.cfg_dir = "turbulence_models/sa/rae2822"
turbmod_sa_bsl_rae2822.cfg_file = "turb_SA_BSL_RAE2822.cfg"
turbmod_sa_bsl_rae2822.test_iter = 20
- turbmod_sa_bsl_rae2822.test_vals = [-3.182935, -0.447793, -0.875861, -3.286652, 0.769925, 0.017709]
+ turbmod_sa_bsl_rae2822.test_vals = [-3.191783, -0.473872, -0.892710, -5.169793, 0.777160, 0.017964]
test_list.append(turbmod_sa_bsl_rae2822)
# SA Negative
@@ -899,7 +899,7 @@ def main():
turbmod_sa_neg_rae2822.cfg_dir = "turbulence_models/sa/rae2822"
turbmod_sa_neg_rae2822.cfg_file = "turb_SA_NEG_RAE2822.cfg"
turbmod_sa_neg_rae2822.test_iter = 10
- turbmod_sa_neg_rae2822.test_vals = [1.570952, 1.355242, -0.869320, 1.244343, 0.452923, 0.000000]
+ turbmod_sa_neg_rae2822.test_vals = [1.429980, 1.127884, 4.865536, 1.277981, 0.472937, 0.000000]
turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.345593, 1.448310, 1.208721, -0.846597, 1.248410, 0.489117, 0.000000]
test_list.append(turbmod_sa_neg_rae2822)
@@ -908,7 +908,7 @@ def main():
turbmod_sa_comp_rae2822.cfg_dir = "turbulence_models/sa/rae2822"
turbmod_sa_comp_rae2822.cfg_file = "turb_SA_COMP_RAE2822.cfg"
turbmod_sa_comp_rae2822.test_iter = 20
- turbmod_sa_comp_rae2822.test_vals = [-3.192776, -0.471890, -0.893254, -5.190537, 0.777261, 0.017904]
+ turbmod_sa_comp_rae2822.test_vals = [-3.190862, -0.473847, -0.893269, -5.195424, 0.777296, 0.017920]
test_list.append(turbmod_sa_comp_rae2822)
# SA Edwards
@@ -916,7 +916,7 @@ def main():
turbmod_sa_edw_rae2822.cfg_dir = "turbulence_models/sa/rae2822"
turbmod_sa_edw_rae2822.cfg_file = "turb_SA_EDW_RAE2822.cfg"
turbmod_sa_edw_rae2822.test_iter = 20
- turbmod_sa_edw_rae2822.test_vals = [-3.198033, -0.439446, -0.883563, -3.899428, 0.786167, 0.017883]
+ turbmod_sa_edw_rae2822.test_vals = [-3.189014, -0.465457, -0.890004, -5.206434, 0.781697, 0.017765]
test_list.append(turbmod_sa_edw_rae2822)
# SA Compressibility and Edwards
@@ -924,7 +924,7 @@ def main():
turbmod_sa_comp_edw_rae2822.cfg_dir = "turbulence_models/sa/rae2822"
turbmod_sa_comp_edw_rae2822.cfg_file = "turb_SA_COMP_EDW_RAE2822.cfg"
turbmod_sa_comp_edw_rae2822.test_iter = 20
- turbmod_sa_comp_edw_rae2822.test_vals = [-2.943295, -0.168387, -0.632480, -5.127730, 0.802507, 0.020196]
+ turbmod_sa_comp_edw_rae2822.test_vals = [-3.056328, -0.293497, -0.766206, -5.230932, 0.798848, 0.019838]
test_list.append(turbmod_sa_comp_edw_rae2822)
# SA QCR
@@ -932,7 +932,7 @@ def main():
turbmod_sa_qcr_rae2822.cfg_dir = "turbulence_models/sa/rae2822"
turbmod_sa_qcr_rae2822.cfg_file = "turb_SA_QCR_RAE2822.cfg"
turbmod_sa_qcr_rae2822.test_iter = 20
- turbmod_sa_qcr_rae2822.test_vals = [-3.056565, -0.419621, -0.805532, -3.857890, 0.760796, 0.016908]
+ turbmod_sa_qcr_rae2822.test_vals = [-3.149635, -0.387144, -0.827745, -2.226502, 0.780050, 0.015548]
test_list.append(turbmod_sa_qcr_rae2822)
############################
@@ -1058,7 +1058,7 @@ def main():
turb_naca0012_2c.cfg_dir = "rans_uq/naca0012"
turb_naca0012_2c.cfg_file = "turb_NACA0012_uq_2c.cfg"
turb_naca0012_2c.test_iter = 10
- turb_naca0012_2c.test_vals = [-5.482691, 1.262918, 0.529450, -0.023537]
+ turb_naca0012_2c.test_vals = [-5.482691, 1.262918, 0.529442, -0.023584]
turb_naca0012_2c.test_vals_aarch64 = [-5.484365, 1.264701, 0.501741, -0.033109]
test_list.append(turb_naca0012_2c)
@@ -1105,7 +1105,7 @@ def main():
hb_rans_preconditioning.cfg_file = "davis.cfg"
hb_rans_preconditioning.test_iter = 25
hb_rans_preconditioning.tol = 0.00001
- hb_rans_preconditioning.test_vals = [-1.905206, 0.481900, 0.599004, 3.605361, -5.945837]
+ hb_rans_preconditioning.test_vals = [-1.905509, 0.482119, 0.598486, 3.605120, -5.946067]
test_list.append(hb_rans_preconditioning)
######################################
@@ -1117,7 +1117,7 @@ def main():
rot_naca0012.cfg_dir = "rotating/naca0012"
rot_naca0012.cfg_file = "rot_NACA0012.cfg"
rot_naca0012.test_iter = 25
- rot_naca0012.test_vals = [-0.023432, 0.083323, 2.000000, -1.181593]
+ rot_naca0012.test_vals = [-0.023360, 0.082942, 2.000000, -1.182142]
test_list.append(rot_naca0012)
# Lid-driven cavity
@@ -1133,7 +1133,7 @@ def main():
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
- spinning_cylinder.test_vals = [-7.471334, -2.007097, 2.183550, 1.847845]
+ spinning_cylinder.test_vals = [-7.471322, -2.007082, 2.183565, 1.847848]
test_list.append(spinning_cylinder)
######################################
@@ -1205,7 +1205,7 @@ def main():
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 20
- edge_VW.test_vals = [-4.444040, 1.757269, -0.000009, 0.000000]
+ edge_VW.test_vals = [-4.478306, 1.723006, -0.000009, 0.000000]
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
@@ -1213,7 +1213,7 @@ def main():
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 20
- edge_PPR.test_vals = [-9.533869, -3.385210, -0.000034, 0.000000]
+ edge_PPR.test_vals = [-8.395110, -2.236894, -0.000034, 0.000000]
test_list.append(edge_PPR)
# Rarefaction Q1D nozzle, include CoolProp fluid model
@@ -1239,7 +1239,7 @@ def main():
datadriven_fluidModel.cfg_dir = "nicf/datadriven"
datadriven_fluidModel.cfg_file = "datadriven_nozzle.cfg"
datadriven_fluidModel.test_iter = 50
- datadriven_fluidModel.test_vals = [-4.879421, -2.353319, -2.344004, 0.390613, -1.559800, 1.322761]
+ datadriven_fluidModel.test_vals = [-6.283594, -3.253961, -4.172935, -0.949415, -2.046039, 1.546933]
test_list.append(datadriven_fluidModel)
######################################
@@ -1268,7 +1268,7 @@ def main():
axial_stage2D.cfg_dir = "turbomachinery/axial_stage_2D"
axial_stage2D.cfg_file = "Axial_stage2D.cfg"
axial_stage2D.test_iter = 20
- axial_stage2D.test_vals = [1.167491, 1.598507, -2.928578, 2.573644, -2.527392, 3.016170, 106370.000000, 106370.000000, 5.726800, 64.383000]
+ axial_stage2D.test_vals = [1.167500, 1.598546, -2.928573, 2.573647, -2.527331, 3.016254, 106370.000000, 106370.000000, 5.726800, 64.383000]
test_list.append(axial_stage2D)
# 2D transonic stator restart
@@ -1316,7 +1316,7 @@ def main():
channel_2D.cfg_dir = "sliding_interface/channel_2D"
channel_2D.cfg_file = "channel_2D_WA.cfg"
channel_2D.test_iter = 2
- channel_2D.test_vals = [2.000000, 0.000000, 0.466215, 0.350091, 0.398996]
+ channel_2D.test_vals = [2.000000, 0.000000, 0.466408, 0.346806, 0.397328]
channel_2D.timeout = 100
channel_2D.unsteady = True
channel_2D.multizone = True
@@ -1327,7 +1327,7 @@ def main():
channel_3D.cfg_dir = "sliding_interface/channel_3D"
channel_3D.cfg_file = "channel_3D_WA.cfg"
channel_3D.test_iter = 2
- channel_3D.test_vals = [2.000000, 0.000000, 0.632256, 0.534230, 0.431926]
+ channel_3D.test_vals = [2.000000, 0.000000, 0.632752, 0.522763, 0.423355]
channel_3D.test_vals_aarch64 = [2.000000, 0.000000, 0.629119, 0.524959, 0.422390]
channel_3D.unsteady = True
channel_3D.multizone = True
@@ -1338,7 +1338,7 @@ def main():
pipe.cfg_dir = "sliding_interface/pipe"
pipe.cfg_file = "pipe_NN.cfg"
pipe.test_iter = 2
- pipe.test_vals = [0.092415, 0.568973, 0.692859, 0.989459, 1.048237]
+ pipe.test_vals = [0.070225, 0.528893, 0.684173, 0.970355, 1.065262]
pipe.unsteady = True
pipe.multizone = True
test_list.append(pipe)
@@ -1348,7 +1348,7 @@ def main():
rotating_cylinders.cfg_dir = "sliding_interface/rotating_cylinders"
rotating_cylinders.cfg_file = "rot_cylinders_WA.cfg"
rotating_cylinders.test_iter = 3
- rotating_cylinders.test_vals = [3.000000, 0.000000, 0.664821, 1.125807, 1.117610]
+ rotating_cylinders.test_vals = [3.000000, 0.000000, 0.686431, 1.159459, 1.151139]
rotating_cylinders.unsteady = True
rotating_cylinders.multizone = True
test_list.append(rotating_cylinders)
@@ -1358,7 +1358,7 @@ def main():
supersonic_vortex_shedding.cfg_dir = "sliding_interface/supersonic_vortex_shedding"
supersonic_vortex_shedding.cfg_file = "sup_vor_shed_WA.cfg"
supersonic_vortex_shedding.test_iter = 5
- supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 0.899643, 1.076189]
+ supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.126036, 1.081775]
supersonic_vortex_shedding.unsteady = True
supersonic_vortex_shedding.multizone = True
test_list.append(supersonic_vortex_shedding)
@@ -1559,7 +1559,7 @@ def main():
pywrapper_naca0012.cfg_dir = "euler/naca0012"
pywrapper_naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
pywrapper_naca0012.test_iter = 80
- pywrapper_naca0012.test_vals = [-5.699819, -5.186257, 0.334856, 0.023343]
+ pywrapper_naca0012.test_vals = [-5.701280, -5.186480, 0.334856, 0.023342]
pywrapper_naca0012.command = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
test_list.append(pywrapper_naca0012)
diff --git a/TestCases/parallel_regression_AD.py b/TestCases/parallel_regression_AD.py
index 26a32c3e2762..ce0c6fd881c5 100644
--- a/TestCases/parallel_regression_AD.py
+++ b/TestCases/parallel_regression_AD.py
@@ -150,7 +150,7 @@ def main():
discadj_axisymmetric_rans_nozzle.cfg_dir = "axisymmetric_rans/air_nozzle"
discadj_axisymmetric_rans_nozzle.cfg_file = "air_nozzle_restart.cfg"
discadj_axisymmetric_rans_nozzle.test_iter = 10
- discadj_axisymmetric_rans_nozzle.test_vals = [9.911310, 5.072379, 7.118130, 2.484452]
+ discadj_axisymmetric_rans_nozzle.test_vals = [9.742490, 5.136585, 7.107742, 2.488366]
discadj_axisymmetric_rans_nozzle.no_restart = True
test_list.append(discadj_axisymmetric_rans_nozzle)
@@ -239,7 +239,7 @@ def main():
discadj_sliding_interface.cfg_dir = "disc_adj_ffi/sliding_interface"
discadj_sliding_interface.cfg_file = "circles.cfg"
discadj_sliding_interface.test_iter = 10
- discadj_sliding_interface.test_vals = [10.000000, -4.395153, -4.419435]
+ discadj_sliding_interface.test_vals = [10.000000, -4.403529, -4.419435]
test_list.append(discadj_sliding_interface)
#######################################################
diff --git a/TestCases/py_wrapper/translating_NACA0012/forces_0.csv.ref b/TestCases/py_wrapper/translating_NACA0012/forces_0.csv.ref
index 3aa219b7120e..0c9091d233ae 100644
--- a/TestCases/py_wrapper/translating_NACA0012/forces_0.csv.ref
+++ b/TestCases/py_wrapper/translating_NACA0012/forces_0.csv.ref
@@ -1,200 +1,200 @@
-199, -0.99, -0.00, 0.00
-0, -2.91, 20.02, 0.00
-1, -4.27, 29.42, 0.00
-2, -5.43, 37.48, 0.00
-3, -6.49, 44.88, 0.00
-4, -7.43, 51.52, 0.00
-5, -8.23, 57.28, 0.00
-6, -8.93, 62.42, 0.00
-7, -9.50, 66.76, 0.00
-8, -9.96, 70.36, 0.00
-9, -10.31, 73.26, 0.00
-10, -10.55, 75.47, 0.00
-11, -10.71, 77.10, 0.00
-12, -10.75, 78.01, 0.00
-13, -10.71, 78.35, 0.00
-14, -10.57, 78.03, 0.00
-15, -10.36, 77.16, 0.00
-16, -10.07, 75.79, 0.00
-17, -9.73, 73.92, 0.00
-18, -9.31, 71.49, 0.00
-19, -8.85, 68.73, 0.00
-20, -8.32, 65.37, 0.00
-21, -7.77, 61.78, 0.00
-22, -7.15, 57.64, 0.00
-23, -6.53, 53.27, 0.00
-24, -5.85, 48.43, 0.00
-25, -5.18, 43.45, 0.00
-26, -4.46, 37.94, 0.00
-27, -3.74, 32.28, 0.00
-28, -2.99, 26.23, 0.00
-29, -2.26, 20.13, 0.00
-30, -1.50, 13.62, 0.00
-31, -0.77, 7.14, 0.00
-32, -0.03, 0.27, 0.00
-33, 0.64, -6.16, 0.00
-34, 1.33, -12.94, 0.00
-35, 1.88, -18.69, 0.00
-36, 2.50, -25.43, 0.00
-37, 2.94, -30.60, 0.00
-38, 3.61, -38.39, 0.00
-39, 4.12, -44.94, 0.00
-40, 5.20, -58.26, 0.00
-41, 6.45, -74.32, 0.00
-42, 8.48, -100.75, 0.00
-43, 10.40, -127.62, 0.00
-44, 12.32, -156.48, 0.00
-45, 14.32, -188.86, 0.00
-46, 15.99, -219.70, 0.00
-47, 17.77, -255.19, 0.00
-48, 19.05, -287.25, 0.00
-49, 20.43, -325.17, 0.00
-50, 21.21, -358.33, 0.00
-51, 21.60, -390.04, 0.00
-52, 20.80, -404.89, 0.00
-53, 19.46, -412.52, 0.00
-54, 17.55, -410.28, 0.00
-55, 15.38, -403.24, 0.00
-56, 12.80, -384.55, 0.00
-57, 10.01, -354.85, 0.00
-58, 7.33, -320.56, 0.00
-59, 5.62, -325.28, 0.00
-60, 4.54, -398.71, 0.00
-61, 2.33, -444.80, 0.00
-62, -0.55, -444.61, 0.00
-63, -3.45, -430.49, 0.00
-64, -6.33, -418.34, 0.00
-65, -9.16, -405.22, 0.00
-66, -11.93, -391.89, 0.00
-67, -14.56, -376.47, 0.00
-68, -17.08, -360.79, 0.00
-69, -19.39, -343.61, 0.00
-70, -21.54, -326.20, 0.00
-71, -23.38, -307.04, 0.00
-72, -25.04, -288.42, 0.00
-73, -26.35, -268.52, 0.00
-74, -27.44, -249.13, 0.00
-75, -28.26, -229.94, 0.00
-76, -28.70, -210.22, 0.00
-77, -28.76, -190.36, 0.00
-78, -28.57, -171.29, 0.00
-79, -27.84, -151.55, 0.00
-80, -26.53, -131.24, 0.00
-81, -24.47, -110.11, 0.00
-82, -22.10, -90.41, 0.00
-83, -17.63, -65.56, 0.00
-84, -13.82, -46.59, 0.00
-85, -9.00, -27.47, 0.00
-86, -3.97, -10.94, 0.00
-87, 2.04, 5.04, 0.00
-88, 8.66, 19.11, 0.00
-89, 17.22, 33.67, 0.00
-90, 26.22, 44.98, 0.00
-91, 38.13, 56.68, 0.00
-92, 50.18, 63.55, 0.00
-93, 64.64, 68.16, 0.00
-94, 81.14, 68.93, 0.00
-95, 92.61, 60.32, 0.00
-96, 98.61, 45.20, 0.00
-97, 91.85, 24.86, 0.00
-98, 60.95, 8.18, 0.00
-99, 54.21, -0.00, 0.00
-100, 87.82, -11.78, 0.00
-101, 110.00, -29.77, 0.00
-102, 92.95, -42.60, 0.00
-103, 73.45, -47.84, 0.00
-104, 54.95, -46.68, 0.00
-105, 39.22, -41.36, 0.00
-106, 29.77, -37.70, 0.00
-107, 13.13, -19.52, 0.00
-108, 1.46, -2.51, 0.00
-109, -12.03, 23.53, 0.00
-110, -21.14, 46.66, 0.00
-111, -30.42, 75.21, 0.00
-112, -36.34, 100.05, 0.00
-113, -42.50, 129.72, 0.00
-114, -45.24, 152.58, 0.00
-115, -47.68, 177.27, 0.00
-116, -48.11, 196.85, 0.00
-117, -49.30, 221.84, 0.00
-118, -49.86, 246.67, 0.00
-119, -50.26, 273.55, 0.00
-120, -49.99, 299.73, 0.00
-121, -49.24, 325.87, 0.00
-122, -47.80, 350.18, 0.00
-123, -46.06, 374.79, 0.00
-124, -43.92, 398.75, 0.00
-125, -41.45, 422.34, 0.00
-126, -38.71, 445.76, 0.00
-127, -35.65, 468.20, 0.00
-128, -32.39, 490.54, 0.00
-129, -28.90, 511.99, 0.00
-130, -25.24, 533.17, 0.00
-131, -21.41, 553.63, 0.00
-132, -17.46, 573.42, 0.00
-133, -13.40, 592.80, 0.00
-134, -9.25, 611.37, 0.00
-135, -5.04, 629.20, 0.00
-136, -0.80, 646.64, 0.00
-137, 3.47, 662.94, 0.00
-138, 7.73, 678.10, 0.00
-139, 11.96, 692.64, 0.00
-140, 16.15, 706.26, 0.00
-141, 20.27, 718.38, 0.00
-142, 24.31, 730.12, 0.00
-143, 28.27, 741.00, 0.00
-144, 32.10, 750.49, 0.00
-145, 35.79, 758.77, 0.00
-146, 39.36, 766.12, 0.00
-147, 42.77, 772.47, 0.00
-148, 46.02, 777.49, 0.00
-149, 49.12, 781.76, 0.00
-150, 52.03, 784.73, 0.00
-151, 54.76, 786.49, 0.00
-152, 57.27, 786.70, 0.00
-153, 59.65, 786.61, 0.00
-154, 62.04, 787.97, 0.00
-155, 63.93, 784.13, 0.00
-156, 65.88, 782.40, 0.00
-157, 67.06, 772.81, 0.00
-158, 69.82, 782.23, 0.00
-159, 35.12, 383.21, 0.00
-160, -13.10, -139.35, 0.00
-161, -9.96, -103.51, 0.00
-162, -7.72, -78.42, 0.00
-163, -7.29, -72.50, 0.00
-164, -7.05, -68.73, 0.00
-165, -6.60, -63.13, 0.00
-166, -6.57, -61.71, 0.00
-167, -6.59, -60.74, 0.00
-168, -6.81, -61.72, 0.00
-169, -7.08, -63.08, 0.00
-170, -7.42, -65.08, 0.00
-171, -7.76, -67.01, 0.00
-172, -8.15, -69.40, 0.00
-173, -8.55, -71.76, 0.00
-174, -8.94, -73.94, 0.00
-175, -9.30, -75.91, 0.00
-176, -9.67, -77.93, 0.00
-177, -10.01, -79.65, 0.00
-178, -10.32, -81.15, 0.00
-179, -10.61, -82.44, 0.00
-180, -10.85, -83.37, 0.00
-181, -11.06, -84.05, 0.00
-182, -11.21, -84.33, 0.00
-183, -11.31, -84.26, 0.00
-184, -11.35, -83.81, 0.00
-185, -11.34, -82.98, 0.00
-186, -11.25, -81.65, 0.00
-187, -11.11, -80.01, 0.00
-188, -10.89, -77.90, 0.00
-189, -10.54, -74.91, 0.00
-190, -10.09, -71.22, 0.00
-191, -9.54, -66.99, 0.00
-192, -8.89, -62.12, 0.00
-193, -8.13, -56.59, 0.00
-194, -7.28, -50.53, 0.00
-195, -6.31, -43.67, 0.00
-196, -5.23, -36.08, 0.00
-197, -4.05, -27.89, 0.00
-198, -2.67, -18.38, 0.00
+199, -0.94, -0.00, 0.00
+0, -2.79, 19.21, 0.00
+1, -4.07, 28.05, 0.00
+2, -5.12, 35.35, 0.00
+3, -6.07, 41.99, 0.00
+4, -6.89, 47.80, 0.00
+5, -7.57, 52.73, 0.00
+6, -8.16, 57.03, 0.00
+7, -8.63, 60.64, 0.00
+8, -8.99, 63.49, 0.00
+9, -9.25, 65.69, 0.00
+10, -9.40, 67.22, 0.00
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diff --git a/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref b/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref
index 1c87fcffcb67..5168d86660a2 100644
--- a/TestCases/py_wrapper/updated_moving_frame_NACA12/forces_0.csv.ref
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+77, -32.48, -214.97, 0.00
+78, -32.01, -191.95, 0.00
+79, -31.12, -169.41, 0.00
+80, -29.76, -147.23, 0.00
+81, -28.42, -127.89, 0.00
+82, -26.46, -108.25, 0.00
+83, -25.23, -93.79, 0.00
+84, -23.18, -78.17, 0.00
+85, -22.06, -67.33, 0.00
+86, -20.11, -55.36, 0.00
+87, -17.52, -43.33, 0.00
+88, -14.90, -32.88, 0.00
+89, -7.49, -14.65, 0.00
+90, -1.78, -3.05, 0.00
+91, 11.94, 17.75, 0.00
+92, 21.51, 27.24, 0.00
+93, 37.02, 39.03, 0.00
+94, 47.69, 40.51, 0.00
+95, 60.96, 39.71, 0.00
+96, 70.98, 32.53, 0.00
+97, 78.52, 21.25, 0.00
+98, 83.66, 11.23, 0.00
+99, 49.17, -0.00, 0.00
+100, 124.12, -16.66, 0.00
+101, 184.07, -49.82, 0.00
+102, 164.48, -75.39, 0.00
+103, 133.69, -87.08, 0.00
+104, 109.43, -92.96, 0.00
+105, 76.86, -81.04, 0.00
+106, 57.12, -72.34, 0.00
+107, 33.93, -50.44, 0.00
+108, 19.70, -33.80, 0.00
+109, 3.84, -7.50, 0.00
+110, -6.08, 13.41, 0.00
+111, -17.27, 42.71, 0.00
+112, -24.34, 67.01, 0.00
+113, -32.29, 98.57, 0.00
+114, -37.23, 125.57, 0.00
+115, -42.27, 157.13, 0.00
+116, -45.00, 184.10, 0.00
+117, -47.22, 212.46, 0.00
+118, -48.02, 237.54, 0.00
+119, -48.54, 264.19, 0.00
+120, -48.03, 288.01, 0.00
+121, -47.18, 312.25, 0.00
+122, -45.73, 334.99, 0.00
+123, -43.96, 357.74, 0.00
+124, -41.77, 379.29, 0.00
+125, -39.34, 400.82, 0.00
+126, -36.68, 422.40, 0.00
+127, -33.75, 443.26, 0.00
+128, -30.64, 464.03, 0.00
+129, -27.30, 483.59, 0.00
+130, -23.83, 503.39, 0.00
+131, -20.19, 522.07, 0.00
+132, -16.46, 540.78, 0.00
+133, -12.62, 558.35, 0.00
+134, -8.71, 575.65, 0.00
+135, -4.74, 591.58, 0.00
+136, -0.75, 607.73, 0.00
+137, 3.26, 622.30, 0.00
+138, 7.25, 636.34, 0.00
+139, 11.22, 649.44, 0.00
+140, 15.14, 662.10, 0.00
+141, 18.99, 673.05, 0.00
+142, 22.76, 683.64, 0.00
+143, 26.45, 693.25, 0.00
+144, 30.01, 701.79, 0.00
+145, 33.44, 708.94, 0.00
+146, 36.75, 715.33, 0.00
+147, 39.92, 720.85, 0.00
+148, 42.91, 725.05, 0.00
+149, 45.76, 728.29, 0.00
+150, 48.36, 729.34, 0.00
+151, 50.65, 727.41, 0.00
+152, 53.13, 729.86, 0.00
+153, 53.65, 707.51, 0.00
+154, 41.35, 525.16, 0.00
+155, -10.50, -128.78, 0.00
+156, -10.40, -123.56, 0.00
+157, -0.38, -4.42, 0.00
+158, 0.07, 0.74, 0.00
+159, -0.56, -6.11, 0.00
+160, -0.06, -0.63, 0.00
+161, 0.35, 3.66, 0.00
+162, 0.54, 5.47, 0.00
+163, 0.57, 5.63, 0.00
+164, 0.50, 4.88, 0.00
+165, 0.34, 3.29, 0.00
+166, 0.13, 1.18, 0.00
+167, -0.18, -1.65, 0.00
+168, -0.56, -5.04, 0.00
+169, -1.04, -9.24, 0.00
+170, -1.56, -13.68, 0.00
+171, -2.17, -18.73, 0.00
+172, -2.78, -23.65, 0.00
+173, -3.45, -28.94, 0.00
+174, -4.09, -33.84, 0.00
+175, -4.78, -39.02, 0.00
+176, -5.44, -43.83, 0.00
+177, -6.12, -48.67, 0.00
+178, -6.74, -52.99, 0.00
+179, -7.38, -57.30, 0.00
+180, -7.94, -61.00, 0.00
+181, -8.47, -64.36, 0.00
+182, -8.92, -67.13, 0.00
+183, -9.27, -69.09, 0.00
+184, -9.56, -70.59, 0.00
+185, -9.71, -71.08, 0.00
+186, -9.80, -71.10, 0.00
+187, -9.76, -70.26, 0.00
+188, -9.64, -68.96, 0.00
+189, -9.45, -67.16, 0.00
+190, -9.17, -64.76, 0.00
+191, -8.82, -61.96, 0.00
+192, -8.34, -58.34, 0.00
+193, -7.78, -54.14, 0.00
+194, -7.08, -49.13, 0.00
+195, -6.24, -43.17, 0.00
+196, -5.26, -36.30, 0.00
+197, -4.14, -28.53, 0.00
+198, -2.87, -19.79, 0.00
diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py
index e1a826cbf170..bec8d64689f8 100755
--- a/TestCases/serial_regression.py
+++ b/TestCases/serial_regression.py
@@ -103,7 +103,7 @@ def main():
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 20
- naca0012.test_vals = [-4.032065, -3.525196, 0.273051, 0.009680]
+ naca0012.test_vals = [-4.031446, -3.524530, 0.273056, 0.009703]
test_list.append(naca0012)
# NACA0012 - FMG test
@@ -111,7 +111,7 @@ def main():
naca0012_FMG.cfg_dir = "euler/naca0012"
naca0012_FMG.cfg_file = "inv_NACA0012.cfg"
naca0012_FMG.test_iter = 20
- naca0012_FMG.test_vals = [-4.160277, -3.553897, 0.296156, 0.016889]
+ naca0012_FMG.test_vals = [-4.160287, -3.553906, 0.296154, 0.016890]
test_list.append(naca0012_FMG)
# Supersonic wedge
@@ -119,7 +119,7 @@ def main():
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 20
- wedge.test_vals = [-4.399745, 1.331048, -0.249527, 0.043953]
+ wedge.test_vals = [-4.359580, 1.370530, -0.249526, 0.043953]
test_list.append(wedge)
# ONERA M6 Wing
@@ -127,7 +127,7 @@ def main():
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
- oneram6.test_vals = [-4.825465, -4.205219, 0.277033, 0.006614]
+ oneram6.test_vals = [-4.825509, -4.205271, 0.277086, 0.006619]
oneram6.timeout = 9600
test_list.append(oneram6)
@@ -145,7 +145,7 @@ def main():
polar_naca0012.cfg_file = "inv_NACA0012.cfg"
polar_naca0012.polar = True
polar_naca0012.test_iter = 10
- polar_naca0012.test_vals = [-1.311660, 4.165589, 0.000067, 0.113157]
+ polar_naca0012.test_vals = [-1.311796, 4.165508, 0.000092, 0.113306]
polar_naca0012.test_vals_aarch64 = [-1.063447, 4.401847, 0.000291, 0.031696]
polar_naca0012.command = TestCase.Command(exec = "compute_polar.py", param = "-n 1 -i 11")
# flaky test on arm64
@@ -157,7 +157,7 @@ def main():
bluntbody.cfg_dir = "euler/bluntbody"
bluntbody.cfg_file = "blunt.cfg"
bluntbody.test_iter = 20
- bluntbody.test_vals = [0.666162, 7.055023, -0.000093, 3.916825]
+ bluntbody.test_vals = [0.565185, 6.945875, 0.000007, 1.970309]
test_list.append(bluntbody)
##########################
@@ -184,7 +184,7 @@ def main():
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
- cylinder.test_vals = [-8.725123, -3.234819, -0.028022, 1.605527, 0.000000]
+ cylinder.test_vals = [-8.725171, -3.234867, -0.028017, 1.605526, 0.000000]
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
@@ -228,7 +228,7 @@ def main():
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 20
- rae2822_sa.test_vals = [-3.131221, -5.161756, 0.778275, 0.019566, 1000.000000]
+ rae2822_sa.test_vals = [-3.056253, -5.155475, 0.783190, 0.020552, 1000.000000]
test_list.append(rae2822_sa)
# RAE2822 SST
@@ -236,7 +236,7 @@ def main():
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 20
- rae2822_sst.test_vals = [-1.745363, -1.484660, 5.883796, 0.579910, 0.017299, 100.000000]
+ rae2822_sst.test_vals = [-1.916371, -1.461911, 5.894621, 0.611793, 0.016873, 100.000000]
test_list.append(rae2822_sst)
# RAE2822 SST_SUST
@@ -244,7 +244,7 @@ def main():
rae2822_sst_sust.cfg_dir = "rans/rae2822"
rae2822_sst_sust.cfg_file = "turb_SST_SUST_RAE2822.cfg"
rae2822_sst_sust.test_iter = 20
- rae2822_sst_sust.test_vals = [-2.464319, 5.852571, 0.490309, 0.042521]
+ rae2822_sst_sust.test_vals = [-2.464309, 5.852571, 0.490309, 0.042519]
test_list.append(rae2822_sst_sust)
# Flat plate
@@ -284,7 +284,7 @@ def main():
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
- turb_oneram6.test_vals = [-2.418713, -6.631577, 0.238587, 0.159599, 0.000000]
+ turb_oneram6.test_vals = [-2.419977, -6.631993, 0.238577, 0.159694, 0.000000]
turb_oneram6.timeout = 3200
test_list.append(turb_oneram6)
@@ -367,7 +367,7 @@ def main():
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
axi_rans_air_nozzle_restart.cfg_file = "air_nozzle_restart.cfg"
axi_rans_air_nozzle_restart.test_iter = 10
- axi_rans_air_nozzle_restart.test_vals = [-2.662936, 2.911899, -2.338516, 2.161131, 0.000000]
+ axi_rans_air_nozzle_restart.test_vals = [-5.135350, 0.436347, -2.878865, 1.663300, 0.000000]
axi_rans_air_nozzle_restart.test_vals_aarch64 = [-14.143715, -9.170705, -10.848554, -5.776746, 0.000000]
axi_rans_air_nozzle_restart.tol = 0.0001
test_list.append(axi_rans_air_nozzle_restart)
@@ -377,7 +377,7 @@ def main():
axi_rans_air_nozzle_species.cfg_dir = "axisymmetric_rans/air_nozzle"
axi_rans_air_nozzle_species.cfg_file = "air_nozzle_species.cfg"
axi_rans_air_nozzle_species.test_iter = 10
- axi_rans_air_nozzle_species.test_vals = [-1.676190, 3.896581, -2.912396, 5.762790, -3.565909, 0.000000]
+ axi_rans_air_nozzle_species.test_vals = [-2.243181, 3.273075, -1.958732, 5.883857, -2.469621, 0.000000]
axi_rans_air_nozzle_species.tol = 0.0001
test_list.append(axi_rans_air_nozzle_species)
@@ -744,7 +744,7 @@ def main():
turb_naca0012_1c.cfg_dir = "rans_uq/naca0012"
turb_naca0012_1c.cfg_file = "turb_NACA0012_uq_1c.cfg"
turb_naca0012_1c.test_iter = 10
- turb_naca0012_1c.test_vals = [-4.981181, 1.343583, 0.597121, 0.017223]
+ turb_naca0012_1c.test_vals = [-4.981181, 1.343583, 0.597111, 0.017244]
turb_naca0012_1c.test_vals_aarch64 = [-4.992791, 1.342873, 0.557941, 0.003269]
test_list.append(turb_naca0012_1c)
@@ -798,7 +798,7 @@ def main():
hb_rans_preconditioning.cfg_dir = "harmonic_balance/hb_rans_preconditioning"
hb_rans_preconditioning.cfg_file = "davis.cfg"
hb_rans_preconditioning.test_iter = 25
- hb_rans_preconditioning.test_vals = [-1.905206, 0.481900, 0.599004, 3.605363, -5.945837]
+ hb_rans_preconditioning.test_vals = [-1.905509, 0.482119, 0.598486, 3.605121, -5.946067]
test_list.append(hb_rans_preconditioning)
######################################
@@ -810,7 +810,7 @@ def main():
rot_naca0012.cfg_dir = "rotating/naca0012"
rot_naca0012.cfg_file = "rot_NACA0012.cfg"
rot_naca0012.test_iter = 25
- rot_naca0012.test_vals = [-1.242808, 4.266616, -0.022207, 0.084206, 2.000000, -1.252601]
+ rot_naca0012.test_vals = [-1.240352, 4.268727, -0.022164, 0.083891, 2.000000, -1.253214]
test_list.append(rot_naca0012)
# Lid-driven cavity
@@ -928,7 +928,7 @@ def main():
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 20
- edge_VW.test_vals = [-8.395792, -2.198370, -0.000009, 0.000000]
+ edge_VW.test_vals = [-8.901513, -2.707051, -0.000009, 0.000000]
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
@@ -936,7 +936,7 @@ def main():
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 20
- edge_PPR.test_vals = [-12.584167, -6.372084, -0.000034, 0.000000]
+ edge_PPR.test_vals = [-12.051551, -5.877885, -0.000034, 0.000000]
test_list.append(edge_PPR)
@@ -966,7 +966,7 @@ def main():
axial_stage2D.cfg_dir = "turbomachinery/axial_stage_2D"
axial_stage2D.cfg_file = "Axial_stage2D.cfg"
axial_stage2D.test_iter = 20
- axial_stage2D.test_vals = [1.167512, 1.598496, -2.928579, 2.573642, -2.527392, 3.016170, 106370.000000, 106370.000000, 5.726800, 64.383000]
+ axial_stage2D.test_vals = [1.167521, 1.598536, -2.928575, 2.573646, -2.527330, 3.016253, 106370.000000, 106370.000000, 5.726800, 64.383000]
test_list.append(axial_stage2D)
# 2D transonic stator restart
@@ -1025,7 +1025,7 @@ def main():
channel_2D.cfg_dir = "sliding_interface/channel_2D"
channel_2D.cfg_file = "channel_2D_WA.cfg"
channel_2D.test_iter = 2
- channel_2D.test_vals = [2.000000, 0.000000, 0.466202, 0.350093, 0.399014]
+ channel_2D.test_vals = [2.000000, 0.000000, 0.466389, 0.346857, 0.397472]
channel_2D.timeout = 100
channel_2D.unsteady = True
channel_2D.multizone = True
@@ -1036,7 +1036,7 @@ def main():
channel_3D.cfg_dir = "sliding_interface/channel_3D"
channel_3D.cfg_file = "channel_3D_WA.cfg"
channel_3D.test_iter = 1
- channel_3D.test_vals = [1.000000, 0.000000, 0.617237, 0.798808, 0.692608]
+ channel_3D.test_vals = [1.000000, 0.000000, 0.620573, 0.810294, 0.718984]
channel_3D.test_vals_aarch64 = [1.000000, 0.000000, 0.611996, 0.798988, 0.702357]
channel_3D.unsteady = True
channel_3D.multizone = True
@@ -1048,7 +1048,7 @@ def main():
pipe.cfg_dir = "sliding_interface/pipe"
pipe.cfg_file = "pipe_NN.cfg"
pipe.test_iter = 2
- pipe.test_vals = [0.568972, 0.692858, 0.989456, 1.048237]
+ pipe.test_vals = [0.528897, 0.684175, 0.970353, 1.065262]
pipe.unsteady = True
pipe.multizone = True
test_list.append(pipe)
@@ -1058,7 +1058,7 @@ def main():
rotating_cylinders.cfg_dir = "sliding_interface/rotating_cylinders"
rotating_cylinders.cfg_file = "rot_cylinders_WA.cfg"
rotating_cylinders.test_iter = 3
- rotating_cylinders.test_vals = [3.000000, 0.000000, 0.664822, 1.125812, 1.117605]
+ rotating_cylinders.test_vals = [3.000000, 0.000000, 0.686432, 1.159461, 1.151134]
rotating_cylinders.unsteady = True
rotating_cylinders.multizone = True
test_list.append(rotating_cylinders)
@@ -1068,7 +1068,7 @@ def main():
supersonic_vortex_shedding.cfg_dir = "sliding_interface/supersonic_vortex_shedding"
supersonic_vortex_shedding.cfg_file = "sup_vor_shed_WA.cfg"
supersonic_vortex_shedding.test_iter = 5
- supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 0.899641, 1.076189]
+ supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.126036, 1.081775]
supersonic_vortex_shedding.unsteady = True
supersonic_vortex_shedding.multizone = True
test_list.append(supersonic_vortex_shedding)
@@ -1667,7 +1667,7 @@ def main():
pywrapper_naca0012.cfg_dir = "euler/naca0012"
pywrapper_naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
pywrapper_naca0012.test_iter = 20
- pywrapper_naca0012.test_vals = [-4.032065, -3.525196, 0.273051, 0.009680]
+ pywrapper_naca0012.test_vals = [-4.031446, -3.524530, 0.273056, 0.009703]
pywrapper_naca0012.command = TestCase.Command(exec = "SU2_CFD.py", param = "-f")
pywrapper_naca0012.timeout = 1600
pywrapper_naca0012.tol = 0.00001
diff --git a/TestCases/serial_regression_AD.py b/TestCases/serial_regression_AD.py
index 8a0277294406..288f8a47efd3 100644
--- a/TestCases/serial_regression_AD.py
+++ b/TestCases/serial_regression_AD.py
@@ -188,7 +188,7 @@ def main():
discadj_sliding_interface.cfg_dir = "disc_adj_ffi/sliding_interface"
discadj_sliding_interface.cfg_file = "circles.cfg"
discadj_sliding_interface.test_iter = 10
- discadj_sliding_interface.test_vals = [10.000000, -4.395143, -4.419431]
+ discadj_sliding_interface.test_vals = [10.000000, -4.403519, -4.419431]
test_list.append(discadj_sliding_interface)
#######################################################
diff --git a/TestCases/tutorials.py b/TestCases/tutorials.py
index d59aad17bf96..f2e16e6a3dbb 100644
--- a/TestCases/tutorials.py
+++ b/TestCases/tutorials.py
@@ -187,7 +187,7 @@ def main():
tutorial_inv_bump.cfg_dir = "../Tutorials/compressible_flow/Inviscid_Bump"
tutorial_inv_bump.cfg_file = "inv_channel.cfg"
tutorial_inv_bump.test_iter = 0
- tutorial_inv_bump.test_vals = [-1.437425, 4.075857, 0.086038, 0.127546]
+ tutorial_inv_bump.test_vals = [-1.437425, 4.075857, 0.085674, 0.123798]
test_list.append(tutorial_inv_bump)
# Inviscid Wedge
@@ -195,7 +195,7 @@ def main():
tutorial_inv_wedge.cfg_dir = "../Tutorials/compressible_flow/Inviscid_Wedge"
tutorial_inv_wedge.cfg_file = "inv_wedge_HLLC.cfg"
tutorial_inv_wedge.test_iter = 0
- tutorial_inv_wedge.test_vals = [-0.481460, 5.253008, -0.215274, 0.037861]
+ tutorial_inv_wedge.test_vals = [-0.481460, 5.253008, -0.191841, 0.033699]
tutorial_inv_wedge.no_restart = True
test_list.append(tutorial_inv_wedge)
@@ -204,7 +204,7 @@ def main():
tutorial_inv_onera.cfg_dir = "../Tutorials/compressible_flow/Inviscid_ONERAM6"
tutorial_inv_onera.cfg_file = "inv_ONERAM6.cfg"
tutorial_inv_onera.test_iter = 0
- tutorial_inv_onera.test_vals = [-5.204928, -4.597762, 0.256743, 0.113097]
+ tutorial_inv_onera.test_vals = [-5.204928, -4.597762, 0.243530, 0.111160]
tutorial_inv_onera.no_restart = True
test_list.append(tutorial_inv_onera)
@@ -213,7 +213,7 @@ def main():
tutorial_lam_cylinder.cfg_dir = "../Tutorials/compressible_flow/Laminar_Cylinder"
tutorial_lam_cylinder.cfg_file = "lam_cylinder.cfg"
tutorial_lam_cylinder.test_iter = 0
- tutorial_lam_cylinder.test_vals = [-6.162141, -0.699617, -0.080518, 43.028531]
+ tutorial_lam_cylinder.test_vals = [-6.162141, -0.699617, -0.080602, 42.990503]
tutorial_lam_cylinder.no_restart = True
test_list.append(tutorial_lam_cylinder)
@@ -287,7 +287,7 @@ def main():
tutorial_turb_oneram6.cfg_dir = "../Tutorials/compressible_flow/Turbulent_ONERAM6"
tutorial_turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
tutorial_turb_oneram6.test_iter = 0
- tutorial_turb_oneram6.test_vals = [-4.564441, -11.537596, 0.293674, 0.087628]
+ tutorial_turb_oneram6.test_vals = [-4.564441, -11.534937, 0.250153, 0.080951]
test_list.append(tutorial_turb_oneram6)
# NICFD Nozzle
@@ -295,7 +295,7 @@ def main():
tutorial_nicfd_nozzle.cfg_dir = "../Tutorials/compressible_flow/NICFD_nozzle"
tutorial_nicfd_nozzle.cfg_file = "NICFD_nozzle.cfg"
tutorial_nicfd_nozzle.test_iter = 20
- tutorial_nicfd_nozzle.test_vals = [-1.800072, -6.002691, 4.635204, 0.000000, 0.000000]
+ tutorial_nicfd_nozzle.test_vals = [-1.799851, -6.002738, 4.635397, 0.000000, 0.000000]
tutorial_nicfd_nozzle.no_restart = True
test_list.append(tutorial_nicfd_nozzle)
@@ -314,7 +314,7 @@ def main():
tutorial_unst_naca0012.cfg_dir = "../Tutorials/compressible_flow/Unsteady_NACA0012"
tutorial_unst_naca0012.cfg_file = "unsteady_naca0012.cfg"
tutorial_unst_naca0012.test_iter = 520
- tutorial_unst_naca0012.test_vals = [520.000000, 0.000000, -5.292139, 0.000000, 0.306930, 0.787006, 0.001794, 0.011018]
+ tutorial_unst_naca0012.test_vals = [520.000000, 0.000000, -5.292186, 0.000000, 0.304255, 0.792893, 0.001907, 0.010888]
tutorial_unst_naca0012.test_vals_aarch64 = [520, 0, -5.292359, 0, 0.284720, 0.766329, 0.000954, 0.007565]
tutorial_unst_naca0012.unsteady = True
test_list.append(tutorial_unst_naca0012)
@@ -324,7 +324,7 @@ def main():
propeller_var_load.cfg_dir = "../Tutorials/compressible_flow/ActuatorDisk_VariableLoad"
propeller_var_load.cfg_file = "propeller_variable_load.cfg"
propeller_var_load.test_iter = 20
- propeller_var_load.test_vals = [-1.831126, -4.534989, -0.000323, 0.171579]
+ propeller_var_load.test_vals = [-1.831998, -4.534991, -0.000323, 0.171494]
propeller_var_load.timeout = 3200
test_list.append(propeller_var_load)
@@ -335,7 +335,7 @@ def main():
tutorial_design_inv_naca0012.cfg_dir = "../Tutorials/design/Inviscid_2D_Unconstrained_NACA0012"
tutorial_design_inv_naca0012.cfg_file = "inv_NACA0012_basic.cfg"
tutorial_design_inv_naca0012.test_iter = 0
- tutorial_design_inv_naca0012.test_vals = [-3.585391, -2.989014, 0.146155, 0.179374]
+ tutorial_design_inv_naca0012.test_vals = [-3.585391, -2.989014, 0.141838, 0.172252]
tutorial_design_inv_naca0012.no_restart = True
test_list.append(tutorial_design_inv_naca0012)
@@ -344,7 +344,7 @@ def main():
tutorial_design_turb_rae2822.cfg_dir = "../Tutorials/design/Turbulent_2D_Constrained_RAE2822"
tutorial_design_turb_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
tutorial_design_turb_rae2822.test_iter = 0
- tutorial_design_turb_rae2822.test_vals = [-1.700114, -4.941829, 0.205309, 0.184990]
+ tutorial_design_turb_rae2822.test_vals = [-1.700114, -4.941830, 0.161066, 0.170510]
tutorial_design_turb_rae2822.no_restart = True
test_list.append(tutorial_design_turb_rae2822)
diff --git a/TestCases/vandv.py b/TestCases/vandv.py
index 516f51cc5ebd..aa9fb4398d52 100644
--- a/TestCases/vandv.py
+++ b/TestCases/vandv.py
@@ -81,7 +81,7 @@ def main():
swbli_sa.cfg_dir = "vandv/rans/swbli"
swbli_sa.cfg_file = "config_sa.cfg"
swbli_sa.test_iter = 5
- swbli_sa.test_vals = [-11.502718, -10.939184, -12.034284, -10.581169, -16.088844, 0.002242, -1.664946, 1.258100]
+ swbli_sa.test_vals = [-11.504424, -10.941741, -12.049925, -10.586263, -16.090385, 0.002242, -1.614365, 1.340100]
swbli_sa.test_vals_aarch64 = [-11.504424, -10.941741, -12.049925, -10.586263, -16.090385, 0.002242, -1.614365, 1.340100]
test_list.append(swbli_sa)
@@ -91,7 +91,7 @@ def main():
swbli_sst.cfg_dir = "vandv/rans/swbli"
swbli_sst.cfg_file = "config_sst.cfg"
swbli_sst.test_iter = 5
- swbli_sst.test_vals = [-11.319578, -10.641523, -11.224600, -10.150215, -11.407538, -2.637660, 0.001816, -1.839484, -3.514593, 11.136000]
+ swbli_sst.test_vals = [-11.569218, -10.909086, -11.607984, -10.431163, -11.407588, -2.637660, 0.001816, -1.305818, -3.514590, 13.399000]
test_list.append(swbli_sst)
# DSMA661 - SA
diff --git a/UnitTests/SU2_CFD/solvers/under_relaxation_ad_tests.cpp b/UnitTests/SU2_CFD/solvers/under_relaxation_ad_tests.cpp
new file mode 100644
index 000000000000..ee1f8659f124
--- /dev/null
+++ b/UnitTests/SU2_CFD/solvers/under_relaxation_ad_tests.cpp
@@ -0,0 +1,77 @@
+/*!
+ * \file under_relaxation_ad_tests.cpp
+ * \brief Tests density ownership and derivatives in compressible under-relaxation.
+ * \author SU2 Contributors
+ * \version 8.5.0 "Harrier"
+ *
+ * SU2 Project Website: https://su2code.github.io
+ *
+ * The SU2 Project is maintained by the SU2 Foundation
+ * (http://su2foundation.org)
+ *
+ * Copyright 2012-2026, SU2 Contributors (cf. AUTHORS.md)
+ *
+ * SU2 is free software; you can redistribute it and/or
+ * modify it under the terms of the GNU Lesser General Public
+ * License as published by the Free Software Foundation; either
+ * version 2.1 of the License, or (at your option) any later version.
+ *
+ * SU2 is distributed in the hope that it will be useful,
+ * but WITHOUT ANY WARRANTY; without even the implied warranty of
+ * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
+ * Lesser General Public License for more details.
+ *
+ * You should have received a copy of the GNU Lesser General Public
+ * License along with SU2. If not, see .
+ */
+
+#include "catch.hpp"
+#include "../../UnitQuadTestCase.hpp"
+
+TEST_CASE("Compressible under-relaxation owns its AD density values", "[UnderRelaxationAD]") {
+ UnitQuadTestCase test;
+ test.config_options =
+ "SOLVER= EULER\nMESH_FORMAT= RECTANGLE\nMESH_BOX_SIZE= 5,5,5\n"
+ "MARKER_EULER= (x_minus,x_plus,y_minus,y_plus)\n"
+ "TIME_DISCRE_FLOW= EULER_IMPLICIT\nMAX_UPDATE_FLOW= 0.01\n";
+ test.InitConfig();
+ test.InitGeometry();
+ test.InitSolver();
+ auto* solver = static_cast(test.solver[FLOW_SOL]);
+ auto* nodes = solver->GetNodes();
+ for (auto p = 0ul; p < test.geometry->GetnPoint(); ++p)
+ for (auto v = 0u; v < 4; ++v) solver->LinSysSol(p, v) = 0.0;
+
+ for (const bool densityLimited : {true, false}) {
+ su2double rho = 2.0;
+#ifdef CODI_REVERSE_TYPE
+ AD::StartRecording();
+ AD::RegisterInput(rho);
+#else
+ SU2_TYPE::SetDerivative(rho, 1.0);
+#endif
+ nodes->SetSolution(0, 0, rho);
+ nodes->SetSolution(0, 1, 3.0);
+ nodes->SetSolution(0, 2, 0.0);
+ nodes->SetSolution(0, 3, 10.0);
+ solver->LinSysSol(0, 0) = densityLimited ? 0.1 : 0.0;
+ solver->LinSysSol(0, 1) = densityLimited ? 0.2 : 0.0;
+ solver->LinSysSol(0, 3) = densityLimited ? 0.4 : 4.0;
+ solver->ComputeUnderRelaxationFactor(test.config.get());
+ su2double factor = nodes->GetUnderRelaxation(0);
+#ifdef CODI_REVERSE_TYPE
+ AD::RegisterOutput(factor);
+ AD::StopRecording();
+ SU2_TYPE::SetDerivative(factor, 1.0);
+ AD::ComputeAdjoint();
+ const auto derivative = SU2_TYPE::GetDerivative(rho);
+#else
+ const auto derivative = SU2_TYPE::GetDerivative(factor);
+#endif
+ CHECK(SU2_TYPE::GetValue(factor) == Approx(densityLimited ? 0.2 : 0.019375));
+ CHECK(derivative == Approx(densityLimited ? 0.1 : 0.0028125));
+#ifdef CODI_REVERSE_TYPE
+ AD::Reset();
+#endif
+ }
+}
diff --git a/UnitTests/meson.build b/UnitTests/meson.build
index ba3c63afce92..76d85e251574 100644
--- a/UnitTests/meson.build
+++ b/UnitTests/meson.build
@@ -28,11 +28,13 @@ su2_cfd_tests = files(['Common/CConfig_tests.cpp',
# Reverse-mode (algorithmic differentiation) tests:
su2_cfd_tests_ad = files(['Common/simple_ad_test.cpp',
+ 'SU2_CFD/solvers/under_relaxation_ad_tests.cpp',
'SU2_CFD/fluid/CFluidModel_tests_AD.cpp',
'Common/toolboxes/multilayer_perceptron/MLP_Jacobian_tests.cpp'])
# Forward-mode (direct differentiation) tests:
-su2_cfd_tests_dd = files(['Common/simple_directdiff_test.cpp'])
+su2_cfd_tests_dd = files(['Common/simple_directdiff_test.cpp',
+ 'SU2_CFD/solvers/under_relaxation_ad_tests.cpp'])
# -------------------------------------------------------------------------
# End of unit test listings