serial

Author: pcarruscag

TestCases/serial_regression.py

@@ -198,7 +198,7 @@ def main():
     poiseuille_profile.cfg_dir   = "navierstokes/poiseuille"
     poiseuille_profile.cfg_file  = "profile_poiseuille.cfg"
     poiseuille_profile.test_iter = 10
-    poiseuille_profile.test_vals         = [-12.008999, -7.262056, -0.000000, 2.089953]
+    poiseuille_profile.test_vals         = [-12.009004, -7.262034, -0.000000, 2.089953]
     poiseuille_profile.test_vals_aarch64 = [-12.009012, -7.262299, -0.000000, 2.089953] #last 4 columns
     test_list.append(poiseuille_profile)
 
@@ -250,15 +250,15 @@ def main():
     turb_wallfunction_flatplate_sst.cfg_dir   = "wallfunctions/flatplate/compressible_SST"
     turb_wallfunction_flatplate_sst.cfg_file  = "turb_SST_flatplate.cfg"
     turb_wallfunction_flatplate_sst.test_iter = 10
-    turb_wallfunction_flatplate_sst.test_vals = [-4.581446, -1.913566, -1.958042, 0.909602, -1.602844, 1.482035, 10.000000, -1.741580, 0.033323, 0.002425]
+    turb_wallfunction_flatplate_sst.test_vals = [-4.036299, -1.916263, -1.821788, 1.443878, -1.579554, 1.521534, 10.000000, -2.351461, 0.030011, 0.002409]
     test_list.append(turb_wallfunction_flatplate_sst)
 
     # FLAT PLATE, WALL FUNCTIONS, COMPRESSIBLE SA
     turb_wallfunction_flatplate_sa           = TestCase('turb_sa_wallfunction_flatplate')
     turb_wallfunction_flatplate_sa.cfg_dir   = "wallfunctions/flatplate/compressible_SA"
     turb_wallfunction_flatplate_sa.cfg_file  = "turb_SA_flatplate.cfg"
     turb_wallfunction_flatplate_sa.test_iter = 10
-    turb_wallfunction_flatplate_sa.test_vals = [-4.456430, -1.959113, -2.105871, 0.883035, -5.248648, 10.000000, -1.537437, 0.034538, 0.002637]
+    turb_wallfunction_flatplate_sa.test_vals = [-3.585860, -1.859493, -1.508986, 1.892510, -5.259058, 10.000000, -2.551025, -0.296176, 0.002533]
     test_list.append(turb_wallfunction_flatplate_sa)
 
     # ONERA M6 Wing
@@ -275,7 +275,7 @@ 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 = [-12.037293, -16.384159, 1.080346, 0.018385, 20.000000, -3.455719, 20.000000, -4.641238, 0.000000]
+    turb_naca0012_sa.test_vals = [-12.037386, -16.384158, 1.080346, 0.018385, 20.000000, -3.455861, 20.000000, -4.641245, 0.000000]
     turb_naca0012_sa.test_vals_aarch64 = [-12.037297, -16.384158, 1.080346, 0.018385, 20.000000, -3.455886, 20.000000, -4.641247, 0.000000]
     turb_naca0012_sa.timeout   = 3200
     test_list.append(turb_naca0012_sa)
@@ -285,7 +285,7 @@ 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         = [-12.076044, -15.246739, -5.861280, 1.070036, 0.015841, -3.297874, 0.000000]
+    turb_naca0012_sst.test_vals         = [-12.094423, -15.251083, -5.906366, 1.070413, 0.015775, -3.178803, 0.000000]
     turb_naca0012_sst.test_vals_aarch64 = [-12.076068, -15.246740, -5.861280, 1.070036, 0.015841, -3.297854, 0.000000]
     turb_naca0012_sst.timeout   = 3200
     test_list.append(turb_naca0012_sst)
@@ -295,7 +295,7 @@ def main():
     turb_naca0012_sst_2003m.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_2003m.cfg_file  = "turb_NACA0012_sst_2003m.cfg"
     turb_naca0012_sst_2003m.test_iter = 10
-    turb_naca0012_sst_2003m.test_vals = [-7.129452, -10.409135, -3.702101, 1.061316, 0.019081, -2.435608, 0.000000]
+    turb_naca0012_sst_2003m.test_vals = [-7.129622, -10.410728, -3.699440, 1.061671, 0.019047, -2.435494, 0.000000]
     turb_naca0012_sst_2003m.timeout   = 3200
     test_list.append(turb_naca0012_sst_2003m)
 
@@ -304,7 +304,7 @@ def main():
     turb_naca0012_sst_sust_restart.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_sust_restart.cfg_file  = "turb_NACA0012_sst_sust.cfg"
     turb_naca0012_sst_sust_restart.test_iter = 10
-    turb_naca0012_sst_sust_restart.test_vals = [-12.074114, -14.836725, -5.732398, 1.000050, 0.019144, -3.315832]
+    turb_naca0012_sst_sust_restart.test_vals = [-12.080463, -14.837169, -5.733461, 1.000893, 0.019109, -2.634206]
     turb_naca0012_sst_sust_restart.test_vals_aarch64 = [-12.074189, -14.836725, -5.732398, 1.000050, 0.019144, -3.315560]
     turb_naca0012_sst_sust_restart.timeout   = 3200
     test_list.append(turb_naca0012_sst_sust_restart)
@@ -314,7 +314,7 @@ def main():
     turb_naca0012_sst_fixedvalues.cfg_dir   = "rans/naca0012"
     turb_naca0012_sst_fixedvalues.cfg_file  = "turb_NACA0012_sst_fixedvalues.cfg"
     turb_naca0012_sst_fixedvalues.test_iter = 10
-    turb_naca0012_sst_fixedvalues.test_vals = [-5.206627, -10.433897, 0.774232, 1.021995, 0.040553, -3.477594]
+    turb_naca0012_sst_fixedvalues.test_vals = [-5.206619, -10.433888, 0.774232, 1.021995, 0.040553, -3.477598]
     turb_naca0012_sst_fixedvalues.timeout   = 3200
     test_list.append(turb_naca0012_sst_fixedvalues)
 
@@ -336,7 +336,7 @@ 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 = [-14.141124, -9.127773, -10.848877, -5.776854, 0.000000]
+    axi_rans_air_nozzle_restart.test_vals = [-12.067967, -7.554256, -8.815999, -3.734660, 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)
@@ -678,7 +678,7 @@ 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 = [-4.992302, 1.342930, 0.558118, 0.003328]
+    turb_naca0012_1c.test_vals = [-4.985486, 1.344249, 0.601107, 0.015762]
     turb_naca0012_1c.test_vals_aarch64 = [-4.992791, 1.342873, 0.557941, 0.003269]
     test_list.append(turb_naca0012_1c)
 
@@ -687,23 +687,23 @@ 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 = [-5.484718, 1.263401, 0.446364, -0.030455]
+    turb_naca0012_2c.test_vals = [-5.482877, 1.263877, 0.444556, -0.031131]
     test_list.append(turb_naca0012_2c)
 
     # NACA0012 3c
     turb_naca0012_3c           = TestCase('turb_naca0012_3c')
     turb_naca0012_3c.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_3c.cfg_file  = "turb_NACA0012_uq_3c.cfg"
     turb_naca0012_3c.test_iter = 10
-    turb_naca0012_3c.test_vals = [-5.583767, 1.231735, 0.413049, -0.037990]
+    turb_naca0012_3c.test_vals = [-5.583759, 1.231949, 0.428507, -0.034739]
     test_list.append(turb_naca0012_3c)
 
     # NACA0012 p1c1
     turb_naca0012_p1c1           = TestCase('turb_naca0012_p1c1')
     turb_naca0012_p1c1.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c1.cfg_file  = "turb_NACA0012_uq_p1c1.cfg"
     turb_naca0012_p1c1.test_iter = 10
-    turb_naca0012_p1c1.test_vals = [-5.119769, 1.283940, 0.486285, -0.021511]
+    turb_naca0012_p1c1.test_vals = [-5.127653, 1.286134, 0.782715, 0.085312]
     turb_naca0012_p1c1.test_vals_aarch64 = [-5.119942, 1.283920, 0.486264, -0.021518]
     test_list.append(turb_naca0012_p1c1)
 
@@ -712,7 +712,7 @@ def main():
     turb_naca0012_p1c2.cfg_dir   = "rans_uq/naca0012"
     turb_naca0012_p1c2.cfg_file  = "turb_NACA0012_uq_p1c2.cfg"
     turb_naca0012_p1c2.test_iter = 10
-    turb_naca0012_p1c2.test_vals = [-5.548631, 1.236601, 0.419149, -0.040387]
+    turb_naca0012_p1c2.test_vals = [-5.553991, 1.237006, 0.523311, -0.006088]
     test_list.append(turb_naca0012_p1c2)
 
     ######################################
@@ -760,7 +760,7 @@ 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 = [-7.894516, -2.469078, 1.703821, 1.670411]
+    spinning_cylinder.test_vals = [-7.894513, -2.469083, 1.703823, 1.670412]
     test_list.append(spinning_cylinder)
 
     ######################################
@@ -772,7 +772,7 @@ 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 = [-2.560665, -1.175914, 0.062108, 1.399401, 2.220371, 1.399349, 2.218609, 0.000000]
+    square_cylinder.test_vals = [-2.560678, -1.175979, 0.062202, 1.399351, 2.219234, 1.399297, 2.217479, 0.000000]
     square_cylinder.unsteady  = True
     test_list.append(square_cylinder)
 
@@ -808,7 +808,7 @@ def main():
     unst_inc_turb_naca0015_sa.cfg_dir   = "unsteady/pitching_naca0015_rans_inc"
     unst_inc_turb_naca0015_sa.cfg_file  = "config_incomp_turb_sa.cfg"
     unst_inc_turb_naca0015_sa.test_iter = 1
-    unst_inc_turb_naca0015_sa.test_vals = [-3.007635, -6.879809, 1.445300, 0.419281]
+    unst_inc_turb_naca0015_sa.test_vals = [-3.007635, -6.879816, 1.445300, 0.419281]
     unst_inc_turb_naca0015_sa.unsteady  = True
     test_list.append(unst_inc_turb_naca0015_sa)
 
@@ -830,7 +830,7 @@ def main():
     ls89_sa.cfg_dir   = "nicf/LS89"
     ls89_sa.cfg_file  = "turb_SA_PR.cfg"
     ls89_sa.test_iter = 20
-    ls89_sa.test_vals = [-5.050483, -13.371790, 0.174939, 0.430757]
+    ls89_sa.test_vals = [-5.050483, -13.371795, 0.174939, 0.430757]
     test_list.append(ls89_sa)
 
     # Rarefaction shock wave edge_VW
@@ -875,15 +875,15 @@ 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 = [1.084450, 1.526941, -2.895086, 2.607566, -2.479664, 3.063779, 106380.000000, 106380.000000, 5.733600, 64.749000]
+    axial_stage2D.test_vals = [1.084452, 1.526941, -2.895084, 2.607568, -2.479664, 3.063779, 106380.000000, 106380.000000, 5.733600, 64.737000]
     test_list.append(axial_stage2D)
 
     # 2D transonic stator restart
     transonic_stator_restart           = TestCase('transonic_stator_restart')
     transonic_stator_restart.cfg_dir   = "turbomachinery/transonic_stator_2D"
     transonic_stator_restart.cfg_file  = "transonic_stator_restart.cfg"
     transonic_stator_restart.test_iter = 20
-    transonic_stator_restart.test_vals         = [-4.443399, -2.566758, -2.169300, 1.651817, -1.356398, 3.172531, -471620.000000, 94.843000, -0.044668]
+    transonic_stator_restart.test_vals         = [-4.443401, -2.566759, -2.169302, 1.651815, -1.356398, 3.172527, -471620.000000, 94.843000, -0.044669]
     transonic_stator_restart.test_vals_aarch64 = [-4.443401, -2.566759, -2.169302, 1.651815, -1.356398, 3.172527, -471620.000000, 94.843000, -0.044669]
     test_list.append(transonic_stator_restart)
 
@@ -913,7 +913,7 @@ def main():
     uniform_flow.cfg_dir   = "sliding_interface/uniform_flow"
     uniform_flow.cfg_file  = "uniform_NN.cfg"
     uniform_flow.test_iter = 2
-    uniform_flow.test_vals = [2.000000, 0.000000, -0.230641, -13.249972]
+    uniform_flow.test_vals = [2.000000, 0.000000, -0.230641, -13.245776]
     uniform_flow.test_vals_aarch64 = [2.000000, 0.000000, -0.230641, -13.249000]
     uniform_flow.tol       = 0.000001
     uniform_flow.unsteady  = True
@@ -1073,7 +1073,7 @@ def main():
     dyn_fsi.cfg_dir   = "fea_fsi/dyn_fsi"
     dyn_fsi.cfg_file  = "config.cfg"
     dyn_fsi.test_iter = 4
-    dyn_fsi.test_vals = [-4.330728, -4.152995, 0.000000, 85.000000]
+    dyn_fsi.test_vals = [-4.330728, -4.152995, 0.000000, 86.000000]
     dyn_fsi.multizone = True
     dyn_fsi.unsteady  = True
     test_list.append(dyn_fsi)
@@ -1534,7 +1534,7 @@ 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         = [-12.076044, -15.246739, -5.861280, 1.070036, 0.015841, -3.297874, 0.000000]
+    pywrapper_turb_naca0012_sst.test_vals         = [-12.094423, -15.251083, -5.906366, 1.070413, 0.015775, -3.178803, 0.000000]
     pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.076068, -15.246740, -5.861280, 1.070036, 0.015841, -3.297854, 0.000000]
     pywrapper_turb_naca0012_sst.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_turb_naca0012_sst.timeout   = 3200
@@ -1548,7 +1548,7 @@ def main():
     pywrapper_square_cylinder.cfg_dir   = "unsteady/square_cylinder"
     pywrapper_square_cylinder.cfg_file  = "turb_square.cfg"
     pywrapper_square_cylinder.test_iter = 3
-    pywrapper_square_cylinder.test_vals = [-2.560665, -1.175914, 0.062108, 1.399401, 2.220371, 1.399349, 2.218609, 0.000000]
+    pywrapper_square_cylinder.test_vals = [-2.560678, -1.175979, 0.062202, 1.399351, 2.219234, 1.399297, 2.217479, 0.000000]
     pywrapper_square_cylinder.command   =  TestCase.Command(exec = "SU2_CFD.py", param = "-f")
     pywrapper_square_cylinder.timeout   = 1600
     pywrapper_square_cylinder.tol       = 0.00001