update regression tests

Author: Bot-Enigma-0

TestCases/hybrid_regression.py

@@ -181,15 +181,15 @@ def main():
     turb_flatplate.cfg_dir   = "rans/flatplate"
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
-    turb_flatplate.test_vals = [-4.316134, -6.737979, -0.187461, 0.057468]
+    turb_flatplate.test_vals = [-4.316127, -6.738720, -0.187461, 0.057469]
     test_list.append(turb_flatplate)
 
     # ONERA M6 Wing
     turb_oneram6           = TestCase('turb_oneram6')
     turb_oneram6.cfg_dir   = "rans/oneram6"
     turb_oneram6.cfg_file  = "turb_ONERAM6.cfg"
     turb_oneram6.test_iter = 10
-    turb_oneram6.test_vals = [-2.408675, -6.662904, 0.238578, 0.158968, 0.000000]
+    turb_oneram6.test_vals = [-2.408655, -6.628338, 0.238580, 0.158951, 0.000000]
     test_list.append(turb_oneram6)
 
     # NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
@@ -238,7 +238,7 @@ def main():
     propeller.cfg_dir   = "rans/propeller"
     propeller.cfg_file  = "propeller.cfg"
     propeller.test_iter = 10
-    propeller.test_vals = [-3.389724, -8.409502, 0.000048, 0.056344]
+    propeller.test_vals = [-3.389724, -8.410479, 0.000048, 0.056344]
     test_list.append(propeller)
 
     #######################################
@@ -332,7 +332,7 @@ 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 = [-1.902111, 0.484080, 0.601469, 3.608991, -5.949369]
+    hb_rans_preconditioning.test_vals = [-1.902098, 0.484244, 0.601482, 3.609005, -5.943887]
     test_list.append(hb_rans_preconditioning)
 
     #############################
@@ -403,7 +403,7 @@ def main():
     inc_turb_naca0012.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012.cfg_file  = "naca0012.cfg"
     inc_turb_naca0012.test_iter = 20
-    inc_turb_naca0012.test_vals = [-4.788405, -11.040560, 0.000008, 0.309505]
+    inc_turb_naca0012.test_vals = [-4.788405, -11.040877, 0.000008, 0.309505]
     test_list.append(inc_turb_naca0012)
 
     # NACA0012, SST_SUST
@@ -503,7 +503,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714713, -5.788302, -0.214960, 0.023758, 0.000000]
+    ddes_flatplate.test_vals = [-2.714713, -5.763293, -0.214960, 0.023758, 0.000000]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 
@@ -582,8 +582,8 @@ def main():
     multi_interface.cfg_dir            = "turbomachinery/multi_interface"
     multi_interface.cfg_file           = "multi_interface_rst.cfg"
     multi_interface.test_iter          = 5
-    multi_interface.test_vals          = [-8.632374, -8.895124, -9.350417]
-    multi_interface.test_vals_aarch64  = [-8.632374, -8.895124, -9.350417]
+    multi_interface.test_vals          = [-8.632229, -8.894737, -9.348730]
+    multi_interface.test_vals_aarch64  = [-8.632229, -8.894737, -9.348730]
     test_list.append(multi_interface)
 
     ######################################

TestCases/hybrid_regression_AD.py

@@ -78,7 +78,7 @@ def main():
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     discadj_rans_naca0012_sa.test_iter = 10
-    discadj_rans_naca0012_sa.test_vals = [-2.997064, -0.196172, 0.000003, -0.000000, 5.000000, -2.919675, 5.000000, -7.323218]
+    discadj_rans_naca0012_sa.test_vals = [-2.997064, -0.197488, 0.000003, -0.000000, 5.000000, -2.919675, 5.000000, -7.318846]
     test_list.append(discadj_rans_naca0012_sa)
 
     # Adjoint turbulent NACA0012 SST
@@ -123,7 +123,7 @@ def main():
     discadj_incomp_turb_NACA0012_sa.cfg_dir   = "disc_adj_incomp_rans/naca0012"
     discadj_incomp_turb_NACA0012_sa.cfg_file  = "turb_naca0012_sa.cfg"
     discadj_incomp_turb_NACA0012_sa.test_iter = 10
-    discadj_incomp_turb_NACA0012_sa.test_vals = [10.000000, -3.845995, -1.031096, 0.000000]
+    discadj_incomp_turb_NACA0012_sa.test_vals = [10.000000, -3.845995, -1.023534, 0.000000]
     test_list.append(discadj_incomp_turb_NACA0012_sa)
 
     # Adjoint Incompressible Turbulent NACA 0012 SST

TestCases/parallel_regression.py

@@ -357,7 +357,7 @@ 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 = [-2.004689, -5.265797, 0.809463, 0.062016, 0]
+    rae2822_sa.test_vals = [-2.004689, -5.265730, 0.809462, 0.062011, 0.000000]
     test_list.append(rae2822_sa)
 
     # RAE2822 SST
@@ -381,15 +381,15 @@ def main():
     turb_flatplate.cfg_dir   = "rans/flatplate"
     turb_flatplate.cfg_file  = "turb_SA_flatplate.cfg"
     turb_flatplate.test_iter = 20
-    turb_flatplate.test_vals = [-4.297198, -6.730442, -0.187632, 0.057700]
+    turb_flatplate.test_vals = [-4.297192, -6.731227, -0.187632, 0.057700]
     test_list.append(turb_flatplate)
 
     # Flat plate (compressible) with species inlet
     turb_flatplate_species           = TestCase('turb_flatplate_species')
     turb_flatplate_species.cfg_dir   = "rans/flatplate"
     turb_flatplate_species.cfg_file  = "turb_SA_flatplate_species.cfg"
     turb_flatplate_species.test_iter = 20
-    turb_flatplate_species.test_vals = [-4.249479, -0.634915, -1.716291, 1.223196, -3.307930, 9.000000, -6.634088, 5.000000, -6.985954, 10.000000, -6.255640, 0.999903, 0.999903]
+    turb_flatplate_species.test_vals = [-4.249474, -0.634908, -1.716288, 1.223201, -3.307930, 9.000000, -6.634095, 5.000000, -6.986784, 10.000000, -6.255641, 0.999903, 0.999903]
     test_list.append(turb_flatplate_species)
 
     # Flat plate SST compressibility correction Wilcox
@@ -413,7 +413,7 @@ def main():
     turb_oneram6.cfg_dir   = "rans/oneram6"
     turb_oneram6.cfg_file  = "turb_ONERAM6.cfg"
     turb_oneram6.test_iter = 10
-    turb_oneram6.test_vals = [-2.408685, -6.662907, 0.238579, 0.158968, 0.000000]
+    turb_oneram6.test_vals = [-2.408664, -6.628340, 0.238581, 0.158952, 0.000000]
     turb_oneram6.timeout   = 3200
     test_list.append(turb_oneram6)
 
@@ -422,7 +422,7 @@ 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 = [-2.282318, -6.614780, 0.234330, 0.143024, 0.000000]
+    turb_oneram6_vc.test_vals = [-2.282278, -6.568458, 0.234350, 0.142989, 0.000000]
     turb_oneram6_vc.timeout = 3200
     test_list.append(turb_oneram6_vc)
 
@@ -431,7 +431,7 @@ 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 = [-4.828066, -4.426250, -11.417591, 0.224679, 0.044309, 1.000000, -0.642977, 31.384000]
+    turb_oneram6_nk.test_vals = [-4.827571, -4.425650, -11.379658, 0.224787, 0.044208, 1.000000, -0.642711, 31.384000]
     turb_oneram6_nk.timeout   = 600
     turb_oneram6_nk.tol       = 0.0001
     test_list.append(turb_oneram6_nk)
@@ -507,7 +507,7 @@ def main():
     propeller.cfg_dir   = "rans/propeller"
     propeller.cfg_file  = "propeller.cfg"
     propeller.test_iter = 10
-    propeller.test_vals = [-3.389724, -8.409502, 0.000048, 0.056344]
+    propeller.test_vals = [-3.389724, -8.410479, 0.000048, 0.056344]
     propeller.timeout   = 3200
     test_list.append(propeller)
 
@@ -646,7 +646,7 @@ def main():
     inc_turb_naca0012.cfg_dir   = "incomp_rans/naca0012"
     inc_turb_naca0012.cfg_file  = "naca0012.cfg"
     inc_turb_naca0012.test_iter = 20
-    inc_turb_naca0012.test_vals = [-4.788595, -11.040625, -0.000002, 0.309519]
+    inc_turb_naca0012.test_vals = [-4.788595, -11.040942, -0.000002, 0.309519]
     test_list.append(inc_turb_naca0012)
 
     # NACA0012, SST_SUST
@@ -732,15 +732,15 @@ 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 = [-2.004689, 0.742306, 0.497308, -5.265797, 0.809463, 0.062016]
+    turbmod_sa_bsl_rae2822.test_vals = [-2.004689, 0.742307, 0.497308, -5.265730, 0.809462, 0.062011]
     test_list.append(turbmod_sa_bsl_rae2822)
 
     # SA Negative
     turbmod_sa_neg_rae2822           = TestCase('turbmod_sa_neg_rae2822')
     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         = [-1.204800, 1.611685, 1.349330, 1.489602, 1.263603, 0.466487, 0]
+    turbmod_sa_neg_rae2822.test_vals         = [-1.345491, 1.448526, 1.208572, -0.846542, 1.263765, 0.494751, 0.000000]
     turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.359612, 1.493629, 1.218367, -1.441703, 1.248499, 0.457987, 0]
     test_list.append(turbmod_sa_neg_rae2822)
 
@@ -749,31 +749,31 @@ 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 = [-2.004687, 0.742304, 0.497309, -5.266084, 0.809467, 0.062029]
+    turbmod_sa_comp_rae2822.test_vals = [-2.004688, 0.742305, 0.497309, -5.266066, 0.809466, 0.062026]
     test_list.append(turbmod_sa_comp_rae2822)
 
     # SA Edwards
     turbmod_sa_edw_rae2822           = TestCase('turbmod_sa_edw_rae2822')
     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 = [-2.004687, 0.742306, 0.497310, -5.290769, 0.809485, 0.062036]
+    turbmod_sa_edw_rae2822.test_vals = [-2.004687, 0.742306, 0.497310, -5.290787, 0.809485, 0.062034]
     test_list.append(turbmod_sa_edw_rae2822)
 
     # SA Compressibility and Edwards
     turbmod_sa_comp_edw_rae2822           = TestCase('turbmod_sa_comp_edw_rae2822')
     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 = [-2.004685, 0.742307, 0.497311, -5.290750, 0.809487, 0.062045]
+    turbmod_sa_comp_edw_rae2822.test_vals = [-2.004686, 0.742307, 0.497311, -5.290776, 0.809487, 0.062044]
     test_list.append(turbmod_sa_comp_edw_rae2822)
 
     # SA QCR
     turbmod_sa_qcr_rae2822           = TestCase('turbmod_sa_qcr_rae2822')
     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 = [-2.004793, 0.742353, 0.497315, -5.265977, 0.807841, 0.062027]
+    turbmod_sa_qcr_rae2822.test_vals = [-2.004794, 0.742354, 0.497315, -5.265910, 0.807835, 0.062022]
     test_list.append(turbmod_sa_qcr_rae2822)
 
     ############################
@@ -785,7 +785,7 @@ def main():
     schubauer_klebanoff_transition.cfg_dir      = "transition/Schubauer_Klebanoff"
     schubauer_klebanoff_transition.cfg_file     = "transitional_BC_model_ConfigFile.cfg"
     schubauer_klebanoff_transition.test_iter    = 10
-    schubauer_klebanoff_transition.test_vals    = [-8.215651, -13.240283, 0.000048, 0.007983]
+    schubauer_klebanoff_transition.test_vals    = [-8.215651, -13.239431, 0.000048, 0.007983]
     test_list.append(schubauer_klebanoff_transition)
 
     #####################################
@@ -942,7 +942,7 @@ 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 = [-1.902098, 0.484070, 0.601481, 3.609002, -5.949356]
+    hb_rans_preconditioning.test_vals = [-1.902085, 0.484234, 0.601494, 3.609016, -5.943874]
     test_list.append(hb_rans_preconditioning)
 
     ######################################
@@ -1009,7 +1009,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714713, -5.788290, -0.214960, 0.023758, 0.000000]
+    ddes_flatplate.test_vals = [-2.714713, -5.763284, -0.214960, 0.023758, 0.000000]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 
@@ -1086,7 +1086,7 @@ def main():
     Aachen_3D_restart.cfg_dir = "turbomachinery/Aachen_turbine"
     Aachen_3D_restart.cfg_file = "aachen_3D_MP_restart.cfg"
     Aachen_3D_restart.test_iter = 5
-    Aachen_3D_restart.test_vals = [-7.701448, -8.512241, -6.014939, -6.468738, -5.801759, -4.607179, -5.551037, -5.300771, -3.804188, -5.256055, -5.765160, -3.609605, -2.229276, -2.883962, -0.563469]
+    Aachen_3D_restart.test_vals = [-7.701447, -8.512235, -6.014939, -6.468414, -5.801735, -4.607179, -5.550688, -5.300764, -3.804188, -5.256009, -5.764984, -3.609605, -2.229276, -2.883960, -0.563469]
     test_list.append(Aachen_3D_restart)
 
     # Jones APU Turbocharger restart
@@ -1119,8 +1119,8 @@ def main():
     multi_interface.cfg_dir            = "turbomachinery/multi_interface"
     multi_interface.cfg_file           = "multi_interface_rst.cfg"
     multi_interface.test_iter          = 5
-    multi_interface.test_vals          = [-8.632374, -8.895124, -9.350417]
-    multi_interface.test_vals_aarch64  = [-8.632374, -8.895124, -9.350417]
+    multi_interface.test_vals          = [-8.632229, -8.894737, -9.348730]
+    multi_interface.test_vals_aarch64  = [-8.632229, -8.894737, -9.348730]
     test_list.append(multi_interface)
 
     ######################################
@@ -1558,7 +1558,7 @@ def main():
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_dir   = "species_transport/venturi_primitive_3species"
     species2_primitiveVenturi_mixingmodel_viscosity.cfg_file  = "species2_primitiveVenturi_mixingmodel_viscosity.cfg"
     species2_primitiveVenturi_mixingmodel_viscosity.test_iter = 50
-    species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-5.232339, -3.617118, -3.857221, -7.533847, -5.126646, 5.000000, -1.682962, 5.000000, -3.474078, 5.000000, -2.086859, 2.495548, 0.985490, 0.600234, 0.909824]
+    species2_primitiveVenturi_mixingmodel_viscosity.test_vals = [-5.236181, -3.624224, -3.871405, -7.533947, -5.128207, 5.000000, -1.678081, 5.000000, -3.489246, 5.000000, -2.086184, 2.495408, 0.985469, 0.600247, 0.909691]
     test_list.append(species2_primitiveVenturi_mixingmodel_viscosity)
 
     # 2 species (1 eq) primitive venturi mixing using mixing model including heat capacity and mass diffusivity

TestCases/parallel_regression_AD.py

@@ -83,7 +83,7 @@ def main():
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     discadj_rans_naca0012_sa.test_iter = 10
-    discadj_rans_naca0012_sa.test_vals = [-2.996963, -0.196020, 0.000004, -0.000000, 5.000000, -3.430615, 5.000000, -7.411381]
+    discadj_rans_naca0012_sa.test_vals = [-2.996963, -0.197337, 0.000004, -0.000000, 5.000000, -3.430615, 5.000000, -7.404064]
     test_list.append(discadj_rans_naca0012_sa)
 
     # Adjoint turbulent NACA0012 SST
@@ -128,8 +128,8 @@ def main():
     discadj_incomp_turb_NACA0012_sa.cfg_dir   = "disc_adj_incomp_rans/naca0012"
     discadj_incomp_turb_NACA0012_sa.cfg_file  = "turb_naca0012_sa.cfg"
     discadj_incomp_turb_NACA0012_sa.test_iter = 10
-    discadj_incomp_turb_NACA0012_sa.test_vals         = [10.000000, -3.846020, -1.031079, 0.000000]
-    discadj_incomp_turb_NACA0012_sa.test_vals_aarch64 = [10.000000, -3.846020, -1.031078, 0.000000]
+    discadj_incomp_turb_NACA0012_sa.test_vals         = [10.000000, -3.846020, -1.023517, 0.000000]
+    discadj_incomp_turb_NACA0012_sa.test_vals_aarch64 = [10.000000, -3.846020, -1.023517, 0.000000]
     test_list.append(discadj_incomp_turb_NACA0012_sa)
 
     # Adjoint Incompressible Turbulent NACA 0012 SST
@@ -256,7 +256,7 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals         = [-1.999668, 0.670563, 0.000000, 0.006210]
+    discadj_heat.test_vals         = [-1.999667, 0.657026, 0.000000, 0.006209]
     discadj_heat.test_vals_aarch64 = [-2.226539, 0.605868, 0.000000, -6.256400]
     test_list.append(discadj_heat)
 

TestCases/serial_regression_AD.py

@@ -78,7 +78,7 @@ def main():
     discadj_rans_naca0012_sa.cfg_dir   = "disc_adj_rans/naca0012"
     discadj_rans_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     discadj_rans_naca0012_sa.test_iter = 10
-    discadj_rans_naca0012_sa.test_vals = [-2.996976, -0.196055, 0.000004, -0.000000, 5.000000, -3.971736, 5.000000, -10.464319]
+    discadj_rans_naca0012_sa.test_vals = [-2.996975, -0.197372, 0.000004, -0.000000, 5.000000, -3.971736, 5.000000, -10.463248]
     test_list.append(discadj_rans_naca0012_sa)
 
     # Adjoint turbulent NACA0012 SST
@@ -183,7 +183,7 @@ def main():
     discadj_heat.cfg_dir   = "disc_adj_heat"
     discadj_heat.cfg_file  = "disc_adj_heat.cfg"
     discadj_heat.test_iter = 10
-    discadj_heat.test_vals = [-2.174678, 0.591525, 0.000000, 0.008748]
+    discadj_heat.test_vals = [-2.174672, 0.581319, 0.000000, 0.008747]
     test_list.append(discadj_heat)
 
     ###################################

TestCases/tutorials.py

@@ -291,7 +291,7 @@ def main():
     tutorial_nicfd_nozzle_pinn.cfg_dir   = "../Tutorials/compressible_flow/NICFD_nozzle/PhysicsInformed"
     tutorial_nicfd_nozzle_pinn.cfg_file  = "config_NICFD_PINN.cfg"
     tutorial_nicfd_nozzle_pinn.test_iter = 20
-    tutorial_nicfd_nozzle_pinn.test_vals = [-3.181747, -1.638856, -1.277037, 2.445964, -11.769570]
+    tutorial_nicfd_nozzle_pinn.test_vals = [-3.181747, -1.638856, -1.277037, 2.445964, -11.759632]
     tutorial_nicfd_nozzle_pinn.no_restart = True
     test_list.append(tutorial_nicfd_nozzle_pinn)
 
@@ -301,7 +301,7 @@ 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, -5.290694, 0.000000, 0.317272, 0.820972, 0.002144, 0.012805]
+    tutorial_unst_naca0012.test_vals         = [520.000000, 0.000000, -5.292632, 0.000000, 0.300303, 0.770888, 0.002399, 0.014070]
     tutorial_unst_naca0012.test_vals_aarch64 = [520.000000, 0.000000, -5.298777, 0.000000, 0.288956, 0.736706, 0.002419, 0.007134]
     tutorial_unst_naca0012.unsteady      = True
     test_list.append(tutorial_unst_naca0012)
@@ -311,7 +311,7 @@ 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 = [-1.830257, -4.535041, -0.000323, 0.171647]
+    propeller_var_load.test_vals = [-1.830257, -4.534990, -0.000323, 0.171646]
     propeller_var_load.timeout   = 3200
     test_list.append(propeller_var_load)