update tests

Author: pcarruscag

TestCases/hybrid_regression.py

@@ -103,32 +103,32 @@ def main():
     flatplate.cfg_dir   = "navierstokes/flatplate"
     flatplate.cfg_file  = "lam_flatplate.cfg"
     flatplate.test_iter = 100
-    flatplate.test_vals = [-7.679131, -2.206953, 0.001084, 0.036233, 2.361500, -2.325300, -1.984700, -1.984700]
+    flatplate.test_vals = [-7.679131, -2.206953, 0.001084, 0.036233, 2.361500, -2.325300, 0, 0]
     test_list.append(flatplate)
 
     # Laminar cylinder (steady)
     cylinder           = TestCase('cylinder')
     cylinder.cfg_dir   = "navierstokes/cylinder"
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
-    cylinder.test_vals = [-8.266513, -2.783904, -0.019899, 1.615668, -0.010207]
+    cylinder.test_vals = [-8.266513, -2.783904, -0.019899, 1.615668, 0]
     test_list.append(cylinder)
 
     # Laminar cylinder (low Mach correction)
     cylinder_lowmach           = TestCase('cylinder_lowmach')
     cylinder_lowmach.cfg_dir   = "navierstokes/cylinder"
     cylinder_lowmach.cfg_file  = "cylinder_lowmach.cfg"
     cylinder_lowmach.test_iter = 25
-    cylinder_lowmach.test_vals         = [-6.830996, -1.368850, -0.143956, 73.963354, 0.002457]
-    cylinder_lowmach.test_vals_aarch64 = [-6.830996, -1.368850, -0.143956, 73.963354, 0.002457]
+    cylinder_lowmach.test_vals         = [-6.830996, -1.368850, -0.143956, 73.963354, 0]
+    cylinder_lowmach.test_vals_aarch64 = [-6.830996, -1.368850, -0.143956, 73.963354, 0]
     test_list.append(cylinder_lowmach)
 
     # 2D Poiseuille flow (body force driven with periodic inlet / outlet)
     poiseuille           = TestCase('poiseuille')
     poiseuille.cfg_dir   = "navierstokes/poiseuille"
     poiseuille.cfg_file  = "lam_poiseuille.cfg"
     poiseuille.test_iter = 10
-    poiseuille.test_vals = [-5.046131, 0.652984, 0.008355, 13.735818, -2.142500]
+    poiseuille.test_vals = [-5.046131, 0.652984, 0.008355, 13.735818, 0]
     test_list.append(poiseuille)
 
     # 2D Poiseuille flow (inlet profile file)
@@ -157,15 +157,15 @@ 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 = [-2.020123, -5.269324, 0.807147, 0.060499, -80602.000000]
+    rae2822_sa.test_vals = [-2.020123, -5.269324, 0.807147, 0.060499, 0]
     test_list.append(rae2822_sa)
 
     # RAE2822 SST
     rae2822_sst           = TestCase('rae2822_sst')
     rae2822_sst.cfg_dir   = "rans/rae2822"
     rae2822_sst.cfg_file  = "turb_SST_RAE2822.cfg"
     rae2822_sst.test_iter = 20
-    rae2822_sst.test_vals = [-0.510363, 4.872736, 0.815617, 0.060920, -73391.000000]
+    rae2822_sst.test_vals = [-0.510363, 4.872736, 0.815617, 0.060920, 0]
     test_list.append(rae2822_sst)
 
     # RAE2822 SST_SUST
@@ -189,24 +189,24 @@ def main():
     turb_oneram6.cfg_dir   = "rans/oneram6"
     turb_oneram6.cfg_file  = "turb_ONERAM6.cfg"
     turb_oneram6.test_iter = 10
-    turb_oneram6.test_vals = [-2.408523, -6.662833, 0.238333, 0.158910, -52718]
+    turb_oneram6.test_vals = [-2.408523, -6.662833, 0.238333, 0.158910, 0]
     test_list.append(turb_oneram6)
 
     # NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
     turb_naca0012_sa           = TestCase('turb_naca0012_sa')
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     turb_naca0012_sa.test_iter = 5
-    turb_naca0012_sa.test_vals         = [-12.098325, -14.149988, 1.057665, 0.022971, 20.000000, -2.292707, 0.000000, -12.068169, -44.871000]
-    turb_naca0012_sa.test_vals_aarch64 = [-12.098325, -14.149988, 1.057665, 0.022971, 20.000000, -2.292707, 0.000000, -12.068169, -44.871000]
+    turb_naca0012_sa.test_vals         = [-12.098325, -14.149988, 1.057665, 0.022971, 20.000000, -2.292707, 0.000000, -12.068169, 0]
+    turb_naca0012_sa.test_vals_aarch64 = [-12.098325, -14.149988, 1.057665, 0.022971, 20.000000, -2.292707, 0.000000, -12.068169, 0]
     test_list.append(turb_naca0012_sa)
 
     # NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
     turb_naca0012_sst           = TestCase('turb_naca0012_sst')
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals = [-12.105781, -15.277738, -6.210248, 1.049757, 0.019249, -2.807857, -38.976000]
+    turb_naca0012_sst.test_vals = [-12.105781, -15.277738, -6.210248, 1.049757, 0.019249, -2.807857, 0]
     test_list.append(turb_naca0012_sst)
 
     # NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
@@ -250,7 +250,7 @@ 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 = [-12.070954, -7.407644, -8.698118, -4.008751, -3572.100000]
+    axi_rans_air_nozzle_restart.test_vals = [-12.070954, -7.407644, -8.698118, -4.008751, 0]
     test_list.append(axi_rans_air_nozzle_restart)
 
     #################################
@@ -381,8 +381,8 @@ def main():
     inc_poly_cylinder.cfg_dir   = "incomp_navierstokes/cylinder"
     inc_poly_cylinder.cfg_file  = "poly_cylinder.cfg"
     inc_poly_cylinder.test_iter = 20
-    inc_poly_cylinder.test_vals         = [-7.851512, -2.093420, 0.029974, 1.921595, -175.300000]
-    inc_poly_cylinder.test_vals_aarch64 = [-7.851510, -2.093419, 0.029974, 1.921595, -175.300000]
+    inc_poly_cylinder.test_vals         = [-7.827942, -2.061513, 0.029525, 1.953498, -174.780000]
+    inc_poly_cylinder.test_vals_aarch64 = [-7.827942, -2.061513, 0.029525, 1.953498, -174.780000]
     test_list.append(inc_poly_cylinder)
 
     # X-coarse laminar bend as a mixed element CGNS test
@@ -452,8 +452,8 @@ def main():
     square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
-    square_cylinder.test_vals = [-2.560839, -1.173497, 0.061188, 1.399403, 2.220575, 1.399351, 2.218781, -0.584690]
-    square_cylinder.test_vals_aarch64 = [-2.557902, -1.173574, 0.058050, 1.399794, 2.220402, 1.399748, 2.218604, -0.453270]
+    square_cylinder.test_vals = [-2.560839, -1.173497, 0.061188, 1.399403, 2.220575, 1.399351, 2.218781, 0]
+    square_cylinder.test_vals_aarch64 = [-2.557902, -1.173574, 0.058050, 1.399794, 2.220402, 1.399748, 2.218604, 0]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
 
@@ -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 = [-2.714785, -5.882681, -0.215041, 0.023758, -617.440000]
+    ddes_flatplate.test_vals = [-2.714785, -5.882681, -0.215041, 0.023758, 0]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 

TestCases/hybrid_regression_AD.py

@@ -110,8 +110,8 @@ def main():
     discadj_incomp_cylinder.cfg_dir   = "disc_adj_incomp_navierstokes/cylinder"
     discadj_incomp_cylinder.cfg_file  = "heated_cylinder.cfg"
     discadj_incomp_cylinder.test_iter = 20
-    discadj_incomp_cylinder.test_vals         = [20.000000, -2.705921, -2.837904, 0.000000]
-    discadj_incomp_cylinder.test_vals_aarch64 = [20.000000, -2.705918, -2.837766, 0.000000]
+    discadj_incomp_cylinder.test_vals         = [20.000000, -2.746353, -2.934792, 0.000000]
+    discadj_incomp_cylinder.test_vals_aarch64 = [20.000000, -2.746353, -2.934792, 0.000000]
     test_list.append(discadj_incomp_cylinder)
 
     ######################################

TestCases/parallel_regression.py

@@ -303,7 +303,7 @@ def main():
     flatplate.cfg_dir   = "navierstokes/flatplate"
     flatplate.cfg_file  = "lam_flatplate.cfg"
     flatplate.test_iter = 100
-    flatplate.test_vals = [-7.613122, -2.140941, 0.001084, 0.036230, 2.361500, -2.325300, -1.975600, -1.975600]
+    flatplate.test_vals = [-7.613122, -2.140941, 0.001084, 0.036230, 2.361500, -2.325300, 0.000000, 0.000000]
     test_list.append(flatplate)
 
     # Custom objective function
@@ -319,23 +319,23 @@ def main():
     cylinder.cfg_dir   = "navierstokes/cylinder"
     cylinder.cfg_file  = "lam_cylinder.cfg"
     cylinder.test_iter = 25
-    cylinder.test_vals = [-8.422091, -2.930561, -0.003396, 1.608418, -0.009920]
+    cylinder.test_vals = [-8.422091, -2.930561, -0.003396, 1.608418, 0.000000]
     test_list.append(cylinder)
 
     # Laminar cylinder (low Mach correction)
     cylinder_lowmach           = TestCase('cylinder_lowmach')
     cylinder_lowmach.cfg_dir   = "navierstokes/cylinder"
     cylinder_lowmach.cfg_file  = "cylinder_lowmach.cfg"
     cylinder_lowmach.test_iter = 25
-    cylinder_lowmach.test_vals = [-6.841604, -1.379532, -1.266739, 76.118218, 0.000274]
+    cylinder_lowmach.test_vals = [-6.841604, -1.379532, -1.266739, 76.118218, 0.000000]
     test_list.append(cylinder_lowmach)
 
     # 2D Poiseuille flow (body force driven with periodic inlet / outlet)
     poiseuille           = TestCase('poiseuille')
     poiseuille.cfg_dir   = "navierstokes/poiseuille"
     poiseuille.cfg_file  = "lam_poiseuille.cfg"
     poiseuille.test_iter = 10
-    poiseuille.test_vals = [-5.050889, 0.648196, 0.000199, 13.639173, -2.114500]
+    poiseuille.test_vals = [-5.050889, 0.648196, 0.000199, 13.639173, 0.000000]
     poiseuille.tol       = 0.001
     test_list.append(poiseuille)
 
@@ -357,15 +357,15 @@ 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, -5.265782, 0.809463, 0.062016, -80576.000000]
+    rae2822_sa.test_vals = [-2.004689, -5.265782, 0.809463, 0.062016, 0.000000]
     test_list.append(rae2822_sa)
 
     # RAE2822 SST
     rae2822_sst           = TestCase('rae2822_sst')
     rae2822_sst.cfg_dir   = "rans/rae2822"
     rae2822_sst.cfg_file  = "turb_SST_RAE2822.cfg"
     rae2822_sst.test_iter = 20
-    rae2822_sst.test_vals = [-0.510369, 4.870643, 0.816647, 0.061833, -71779.000000]
+    rae2822_sst.test_vals = [-0.510369, 4.870643, 0.816647, 0.061833, 0.000000]
     test_list.append(rae2822_sst)
 
     # RAE2822 SST_SUST
@@ -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 = [-2.408532, -6.662836, 0.238334, 0.158910, -52718]
+    turb_oneram6.test_vals = [-2.408532, -6.662836, 0.238334, 0.158910, 0]
     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 = [-2.281896, -6.614616, 0.233785, 0.142861, -47942]
+    turb_oneram6_vc.test_vals = [-2.281896, -6.614616, 0.233785, 0.142861, 0]
     turb_oneram6_vc.timeout = 3200
     test_list.append(turb_oneram6_vc)
 
@@ -441,7 +441,7 @@ def main():
     turb_naca0012_sa.cfg_dir   = "rans/naca0012"
     turb_naca0012_sa.cfg_file  = "turb_NACA0012_sa.cfg"
     turb_naca0012_sa.test_iter = 5
-    turb_naca0012_sa.test_vals = [-12.094721, -14.685268, 1.057665, 0.022971, 20.000000, -1.692925, 20.000000, -4.037672, -44.871000]
+    turb_naca0012_sa.test_vals = [-12.094721, -14.685268, 1.057665, 0.022971, 20.000000, -1.692925, 20.000000, -4.037672, 0]
     turb_naca0012_sa.timeout   = 3200
     test_list.append(turb_naca0012_sa)
 
@@ -450,8 +450,8 @@ def main():
     turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     turb_naca0012_sst.test_iter = 10
-    turb_naca0012_sst.test_vals = [-12.107692, -15.277743, -6.210238, 1.049757, 0.019249, -2.357984, -38.976000]
-    turb_naca0012_sst.test_vals_aarch64 = [-12.107692, -15.277743, -6.210238, 1.049757, 0.019249, -2.357984, -38.976000]
+    turb_naca0012_sst.test_vals = [-12.107692, -15.277743, -6.210238, 1.049757, 0.019249, -2.357984, 0]
+    turb_naca0012_sst.test_vals_aarch64 = [-12.107692, -15.277743, -6.210238, 1.049757, 0.019249, -2.357984, 0]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
 
@@ -530,7 +530,7 @@ 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 = [-12.071395, -7.467871, -8.649076, -3.995810, -3572.100000]
+    axi_rans_air_nozzle_restart.test_vals = [-12.071395, -7.467871, -8.649076, -3.995810, 0]
     axi_rans_air_nozzle_restart.tol       = 0.0001
     test_list.append(axi_rans_air_nozzle_restart)
 
@@ -602,7 +602,7 @@ def main():
     inc_poly_cylinder.cfg_dir   = "incomp_navierstokes/cylinder"
     inc_poly_cylinder.cfg_file  = "poly_cylinder.cfg"
     inc_poly_cylinder.test_iter = 20
-    inc_poly_cylinder.test_vals = [-7.791831, -2.062292, 0.013040, 1.913997, -171.120000]
+    inc_poly_cylinder.test_vals = [-7.786564, -2.036735, 0.012980, 1.944887, -170.930000]
     test_list.append(inc_poly_cylinder)
 
     # X-coarse laminar bend as a mixed element CGNS test
@@ -732,8 +732,8 @@ 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         = [-1.466238, 3.169232, 2.756518, 4.722767, 1.120253, 0.378675, -83444.000000]
-    turbmod_sa_neg_rae2822.test_vals_aarch64 = [-1.359612, 1.493629, 1.218367, -1.441703, 1.248499, 0.457987, -86467.000000]
+    turbmod_sa_neg_rae2822.test_vals         = [-1.466238, 3.169232, 2.756518, 4.722767, 1.120253, 0.378675, 0]
+    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)
 
     # SA Compressibility Correction
@@ -974,7 +974,7 @@ def main():
     square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     square_cylinder.cfg_file  = "turb_square.cfg"
     square_cylinder.test_iter = 3
-    square_cylinder.test_vals = [-1.173495, 0.061186, 1.399404, 2.220578, 1.399352, 2.218783, -0.584750]
+    square_cylinder.test_vals = [-1.173495, 0.061186, 1.399404, 2.220578, 1.399352, 2.218783, 0]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
 
@@ -1001,7 +1001,7 @@ def main():
     ddes_flatplate.cfg_dir   = "ddes/flatplate"
     ddes_flatplate.cfg_file  = "ddes_flatplate.cfg"
     ddes_flatplate.test_iter = 10
-    ddes_flatplate.test_vals = [-2.714785, -5.882679, -0.215041, 0.023758, -617.450000]
+    ddes_flatplate.test_vals = [-2.714785, -5.882679, -0.215041, 0.023758, 0]
     ddes_flatplate.unsteady  = True
     test_list.append(ddes_flatplate)
 
@@ -1282,7 +1282,7 @@ def main():
     p1rad.cfg_dir   = "radiation/p1model"
     p1rad.cfg_file  = "configp1.cfg"
     p1rad.test_iter = 100
-    p1rad.test_vals = [-7.743666, -7.921411, -2.111848, 0.098302, -45.023000]
+    p1rad.test_vals = [-7.743666, -7.921411, -2.111848, 0.098302, -47.897000]
     test_list.append(p1rad)
 
 
@@ -1359,8 +1359,8 @@ def main():
     pywrapper_turb_naca0012_sst.cfg_dir   = "rans/naca0012"
     pywrapper_turb_naca0012_sst.cfg_file  = "turb_NACA0012_sst.cfg"
     pywrapper_turb_naca0012_sst.test_iter = 10
-    pywrapper_turb_naca0012_sst.test_vals = [-12.107692, -15.277743, -6.210238, 1.049757, 0.019249, -2.357984, -38.976000]
-    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.107692, -15.277743, -6.210238, 1.049757, 0.019249, -2.357984, -38.976000]
+    pywrapper_turb_naca0012_sst.test_vals = [-12.107692, -15.277743, -6.210238, 1.049757, 0.019249, -2.357984, 0]
+    pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.107692, -15.277743, -6.210238, 1.049757, 0.019249, -2.357984, 0]
     pywrapper_turb_naca0012_sst.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
     test_list.append(pywrapper_turb_naca0012_sst)
@@ -1370,7 +1370,7 @@ def main():
     pywrapper_square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     pywrapper_square_cylinder.cfg_file  = "turb_square.cfg"
     pywrapper_square_cylinder.test_iter = 10
-    pywrapper_square_cylinder.test_vals = [-1.176405, -0.354027, 1.407859, 2.360784, 1.404715, 2.302615, -0.394750]
+    pywrapper_square_cylinder.test_vals = [-1.176405, -0.354027, 1.407859, 2.360784, 1.404715, 2.302615, 0]
     pywrapper_square_cylinder.command   = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
     pywrapper_square_cylinder.unsteady  = True
     test_list.append(pywrapper_square_cylinder)
@@ -1422,7 +1422,7 @@ def main():
     pywrapper_unsteadyCHT.cfg_dir       = "py_wrapper/flatPlate_unsteady_CHT"
     pywrapper_unsteadyCHT.cfg_file      = "unsteady_CHT_FlatPlate_Conf.cfg"
     pywrapper_unsteadyCHT.test_iter     = 5
-    pywrapper_unsteadyCHT.test_vals     = [-1.614167, 2.240663, -0.001316, 0.177491]
+    pywrapper_unsteadyCHT.test_vals     = [-1.614167, 2.240663, -0.001392, 0.177499]
     pywrapper_unsteadyCHT.command       = TestCase.Command("mpirun -np 2", "python", "launch_unsteady_CHT_FlatPlate.py --parallel -f")
     pywrapper_unsteadyCHT.unsteady      = True
     test_list.append(pywrapper_unsteadyCHT)

TestCases/parallel_regression_AD.py

@@ -116,7 +116,7 @@ def main():
     discadj_incomp_cylinder.cfg_dir   = "disc_adj_incomp_navierstokes/cylinder"
     discadj_incomp_cylinder.cfg_file  = "heated_cylinder.cfg"
     discadj_incomp_cylinder.test_iter = 20
-    discadj_incomp_cylinder.test_vals = [20.000000, -2.195581, -2.162081, 0.000000]
+    discadj_incomp_cylinder.test_vals = [20.000000, -2.082673, -2.013587, 0.000000]
     test_list.append(discadj_incomp_cylinder)
 
     ######################################
@@ -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         = [-2.117791, 0.784475, 0.000000, -0.574700]
+    discadj_heat.test_vals         = [-1.840132, 0.751835, 0.000000, 0.006760]
     discadj_heat.test_vals_aarch64 = [-2.226539, 0.605868, 0.000000, -6.256400]
     test_list.append(discadj_heat)