From 767a5374db6c07bd48d22e584505564a6872a09c Mon Sep 17 00:00:00 2001 From: Pedro Gomes Date: Sun, 29 Sep 2024 17:00:46 -0700 Subject: [PATCH] more updates --- TestCases/hybrid_regression.py | 61 +++++++++++------------- TestCases/parallel_regression.py | 2 +- TestCases/serial_regression.py | 81 ++++++++++++++------------------ 3 files changed, 65 insertions(+), 79 deletions(-) diff --git a/TestCases/hybrid_regression.py b/TestCases/hybrid_regression.py index 23ccc566755..d500696e304 100644 --- a/TestCases/hybrid_regression.py +++ b/TestCases/hybrid_regression.py @@ -59,7 +59,7 @@ def main(): naca0012.cfg_dir = "euler/naca0012" naca0012.cfg_file = "inv_NACA0012_Roe.cfg" naca0012.test_iter = 20 - naca0012.test_vals = [-4.444945, -3.941041, 0.318999, 0.022365] + naca0012.test_vals = [-4.431337, -3.970066, 0.319205, 0.022299] test_list.append(naca0012) # Supersonic wedge @@ -103,8 +103,7 @@ def main(): flatplate.cfg_dir = "navierstokes/flatplate" flatplate.cfg_file = "lam_flatplate.cfg" flatplate.test_iter = 100 - flatplate.test_vals = [-7.700620, -2.229886, 0.001084, 0.036235, 2.361500, -2.325300, -1.823400, -1.823400] - flatplate.test_vals_aarch64 = [-9.154130, -3.663197, 0.001112, 0.036277, 2.361500, -2.325300, -2.278800, -2.278800] + flatplate.test_vals = [-7.679131, -2.206953, 0.001084, 0.036233, 2.361500, -2.325300, -1.984700, -1.984700] test_list.append(flatplate) # Laminar cylinder (steady) @@ -112,8 +111,7 @@ def main(): cylinder.cfg_dir = "navierstokes/cylinder" cylinder.cfg_file = "lam_cylinder.cfg" cylinder.test_iter = 25 - cylinder.test_vals = [-8.265865, -2.783635, -0.019914, 1.614879, -0.010191] - cylinder.test_vals_aarch64 = [-6.765429, -1.297425, 0.019571, 0.310231, 0.123270] + cylinder.test_vals = [-8.266513, -2.783904, -0.019899, 1.615668, -0.010207] test_list.append(cylinder) # Laminar cylinder (low Mach correction) @@ -130,8 +128,7 @@ def main(): poiseuille.cfg_dir = "navierstokes/poiseuille" poiseuille.cfg_file = "lam_poiseuille.cfg" poiseuille.test_iter = 10 - poiseuille.test_vals = [-5.048283, 0.650813, 0.008713, 13.677671, -2.054800] - poiseuille.test_vals_aarch64 = [-5.048282, 0.650814, 0.008713, 13.677691, -2.054800] + poiseuille.test_vals = [-5.046131, 0.652984, 0.008355, 13.735818, -2.142500] test_list.append(poiseuille) # 2D Poiseuille flow (inlet profile file) @@ -148,8 +145,7 @@ def main(): periodic2d.cfg_dir = "navierstokes/periodic2D" periodic2d.cfg_file = "config.cfg" periodic2d.test_iter = 1400 - periodic2d.test_vals = [-10.818509, -8.363386, -8.287481, -5.334812, -1.087925, -2945.200000] - periodic2d.test_vals_aarch64 = [-10.818510, -8.363388, -8.287480, -5.334814, -1.087922, -2945.2] + periodic2d.test_vals = [-10.817611, -8.363544, -8.287460, -5.334104, -1.088411, -2945.2] test_list.append(periodic2d) ########################## @@ -185,7 +181,7 @@ 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 = [-4.156553, -6.736064, -0.176184, 0.057478] + turb_flatplate.test_vals = [-4.312826, -6.736053, -0.187467, 0.057454] test_list.append(turb_flatplate) # ONERA M6 Wing @@ -193,7 +189,7 @@ def main(): turb_oneram6.cfg_dir = "rans/oneram6" turb_oneram6.cfg_file = "turb_ONERAM6.cfg" turb_oneram6.test_iter = 10 - turb_oneram6.test_vals = [-2.392863, -6.689822, 0.230745, 0.158812, -33786.000000] + turb_oneram6.test_vals = [-2.408523, -6.662833, 0.238333, 0.158910, -52718] test_list.append(turb_oneram6) # NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242) @@ -226,8 +222,7 @@ 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 = [-5.192598, -10.042489, -1.617721, 1.022073, 0.040198, -2.381138] - turb_naca0012_sst_fixedvalues.test_vals_aarch64 = [-5.192599, -10.042490, -1.617720, 1.022073, 0.040198, -2.381138] + turb_naca0012_sst_fixedvalues.test_vals = [-5.192504, -10.035367, -1.617698, 1.022029, 0.040310, -2.381926] test_list.append(turb_naca0012_sst_fixedvalues) # NACA0012 (SST, explicit Euler for flow and turbulence equations) @@ -235,7 +230,7 @@ def main(): turb_naca0012_sst_expliciteuler.cfg_dir = "rans/naca0012" turb_naca0012_sst_expliciteuler.cfg_file = "turb_NACA0012_sst_expliciteuler.cfg" turb_naca0012_sst_expliciteuler.test_iter = 10 - turb_naca0012_sst_expliciteuler.test_vals = [-3.532289, -3.157766, 3.364024, 1.122901, 0.500798, -float("inf")] + turb_naca0012_sst_expliciteuler.test_vals = [-3.533827, -3.157766, 3.364024, 1.122856, 0.500771, -float("inf")] test_list.append(turb_naca0012_sst_expliciteuler) # PROPELLER @@ -243,7 +238,7 @@ def main(): propeller.cfg_dir = "rans/propeller" propeller.cfg_file = "propeller.cfg" propeller.test_iter = 10 - propeller.test_vals = [-3.389575, -8.409251, 0.000048, 0.056329] + propeller.test_vals = [-3.389724, -8.409223, 0.000048, 0.056344] test_list.append(propeller) ####################################### @@ -280,7 +275,7 @@ 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 = [-4.980878, 1.138865, 0.247731, -0.117335] + turb_naca0012_1c.test_vals = [-4.976788, 1.141064, 0.246262, -0.116795] turb_naca0012_1c.test_vals_aarch64 = [-4.981105, 1.138873, 0.248013, -0.117248] test_list.append(turb_naca0012_1c) @@ -289,7 +284,7 @@ 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 = [-5.483313, 0.968731, 0.215420, -0.124767] + turb_naca0012_2c.test_vals = [-5.485942, 0.967831, 0.236638, -0.119183] turb_naca0012_2c.test_vals_aarch64 = [-5.483345, 0.968720, 0.214914, -0.124932] test_list.append(turb_naca0012_2c) @@ -298,7 +293,7 @@ def main(): 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 = [-5.584300, 0.931293, 0.207446, -0.125692] + turb_naca0012_3c.test_vals = [-5.584306, 0.931276, 0.226035, -0.120956] turb_naca0012_3c.test_vals_aarch64 = [-5.584300, 0.931293, 0.207447, -0.125691] test_list.append(turb_naca0012_3c) @@ -307,7 +302,7 @@ def main(): 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 = [-5.132363, 1.075634, 0.337251, -0.082829] + turb_naca0012_p1c1.test_vals = [-5.114413, 1.076465, 0.227286, -0.123574] turb_naca0012_p1c1.test_vals_aarch64 = [-5.132358, 1.075658, 0.337268, -0.082827] test_list.append(turb_naca0012_p1c1) @@ -316,7 +311,7 @@ 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 = [-5.554392, 0.943703, 0.229483, -0.121058] + turb_naca0012_p1c2.test_vals = [-5.548780, 0.945778, 0.213968, -0.126040] turb_naca0012_p1c2.test_vals_aarch64 = [-5.554425, 0.943683, 0.229293, -0.121125] test_list.append(turb_naca0012_p1c2) @@ -436,7 +431,7 @@ def main(): cavity.cfg_dir = "moving_wall/cavity" cavity.cfg_file = "lam_cavity.cfg" cavity.test_iter = 25 - cavity.test_vals = [-5.627868, -0.164404, 0.053310, 2.545839] + cavity.test_vals = [-5.627869, -0.164403, 0.054734, 2.545856] test_list.append(cavity) # Spinning cylinder @@ -444,7 +439,7 @@ 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 = [-8.006541, -2.609759, 1.495662, 1.486341] + spinning_cylinder.test_vals = [-8.008048, -2.611074, 1.497289, 1.487468] spinning_cylinder.test_vals_aarch64 = [-8.006541, -2.609759, 1.495662, 1.486341] test_list.append(spinning_cylinder) @@ -457,7 +452,7 @@ 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 = [-2.557949, -1.173575, 0.058030, 1.399794, 2.220402, 1.399748, 2.218603, -0.453270] + 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.unsteady = True test_list.append(square_cylinder) @@ -569,7 +564,7 @@ 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 = [0.983739, 1.534333, -2.888521, 2.606770, -2.418339, 3.087275, 106380.000000, 106380.000000, 5.732600, 64.711000] + axial_stage2D.test_vals = [0.987667, 1.531950, -2.888460, 2.606789, -2.418222, 3.087180, 106380.000000, 106380.000000, 5.733000, 64.728000] axial_stage2D.test_vals_aarch64 = [0.983739, 1.534333, -2.888521, 2.606770, -2.418339, 3.087275, 106380, 106380, 5.7325, 64.711] test_list.append(axial_stage2D) @@ -600,7 +595,7 @@ def main(): uniform_flow.cfg_dir = "sliding_interface/uniform_flow" uniform_flow.cfg_file = "uniform_NN.cfg" uniform_flow.test_iter = 5 - uniform_flow.test_vals = [5.000000, 0.000000, -0.185381, -10.631535] + uniform_flow.test_vals = [5.000000, 0.000000, -0.186037, -10.624438] uniform_flow.unsteady = True uniform_flow.multizone = True test_list.append(uniform_flow) @@ -610,7 +605,7 @@ 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, 0.419762, 0.352170, 0.404385] + channel_2D.test_vals = [2.000000, 0.000000, 0.417392, 0.350483, 0.401514] channel_2D.unsteady = True channel_2D.multizone = True test_list.append(channel_2D) @@ -620,7 +615,7 @@ 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, 0.623108, 0.505077, 0.412801] + channel_3D.test_vals = [2.000000, 0.000000, 0.622653, 0.506145, 0.410984] channel_3D.test_vals_aarch64 = [2.000000, 0.000000, 0.620558, 0.504323, 0.412729] channel_3D.unsteady = True channel_3D.multizone = True @@ -632,7 +627,7 @@ def main(): pipe.cfg_dir = "sliding_interface/pipe" pipe.cfg_file = "pipe_NN.cfg" pipe.test_iter = 2 - pipe.test_vals = [0.116650, 0.481386, 0.648698, 0.982997, 1.018359] + pipe.test_vals = [0.121511, 0.477625, 0.641343, 0.983342, 1.018866] pipe.unsteady = True pipe.multizone = True test_list.append(pipe) @@ -652,7 +647,7 @@ 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, 1.207949, 1.036083] + supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.206774, 1.053443] supersonic_vortex_shedding.unsteady = True supersonic_vortex_shedding.multizone = True test_list.append(supersonic_vortex_shedding) @@ -703,7 +698,7 @@ def main(): fsi2d.cfg_dir = "fea_fsi/WallChannel_2d" fsi2d.cfg_file = "configFSI.cfg" fsi2d.test_iter = 4 - fsi2d.test_vals = [4.000000, 0.000000, -3.729243, -4.153954] + fsi2d.test_vals = [4.000000, 0.000000, -3.726064, -4.277803] fsi2d.multizone= True fsi2d.unsteady = True fsi2d.enabled_with_tsan = False @@ -724,7 +719,7 @@ 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 = [-4.330441, -4.057994, 0.000000, 103.000000] + dyn_fsi.test_vals = [-4.330905, -4.153024, 0.000000, 103.000000] dyn_fsi.test_vals_aarch64 = [-4.332167, -4.057742, 0.000000, 102.000000] dyn_fsi.multizone = True dyn_fsi.unsteady = True @@ -735,7 +730,7 @@ def main(): stat_fsi_restart.cfg_dir = "fea_fsi/stat_fsi" stat_fsi_restart.cfg_file = "config_restart.cfg" stat_fsi_restart.test_iter = 1 - stat_fsi_restart.test_vals = [-3.463348, -4.232710, 0.000000, 37.000000] + stat_fsi_restart.test_vals = [-3.468782, -4.271197, 0.000000, 36.000000] stat_fsi_restart.test_vals_aarch64 = [-3.442878, -4.228058, 0.000000, 37.000000] stat_fsi_restart.multizone = True test_list.append(stat_fsi_restart) @@ -749,7 +744,7 @@ def main(): mms_fvm_ns.cfg_dir = "mms/fvm_navierstokes" mms_fvm_ns.cfg_file = "lam_mms_roe.cfg" mms_fvm_ns.test_iter = 20 - mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000] + mms_fvm_ns.test_vals = [-2.808514, 2.152655, 0.000000, 0.000000] test_list.append(mms_fvm_ns) # FVM, incompressible, euler diff --git a/TestCases/parallel_regression.py b/TestCases/parallel_regression.py index d406e929b41..abb4e1d4d8d 100644 --- a/TestCases/parallel_regression.py +++ b/TestCases/parallel_regression.py @@ -889,7 +889,7 @@ 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 = [-5.484979, 0.968118, 0.320621, -0.114603]\ + turb_naca0012_2c.test_vals = [-5.484979, 0.968118, 0.320621, -0.114603] test_list.append(turb_naca0012_2c) # NACA0012 3c diff --git a/TestCases/serial_regression.py b/TestCases/serial_regression.py index e5825f786e1..229e747f820 100644 --- a/TestCases/serial_regression.py +++ b/TestCases/serial_regression.py @@ -101,7 +101,7 @@ def main(): naca0012.cfg_dir = "euler/naca0012" naca0012.cfg_file = "inv_NACA0012_Roe.cfg" naca0012.test_iter = 20 - naca0012.test_vals = [-4.444941, -3.941038, 0.318998, 0.022365] + naca0012.test_vals = [-4.431325, -3.970055, 0.319205, 0.022299] test_list.append(naca0012) # Supersonic wedge @@ -166,7 +166,7 @@ def main(): flatplate.cfg_dir = "navierstokes/flatplate" flatplate.cfg_file = "lam_flatplate.cfg" flatplate.test_iter = 20 - flatplate.test_vals = [-5.122306, 0.357174, 0.001311, 0.028230, 2.361600, -2.333300, -2.629100, -2.629100] + flatplate.test_vals = [-5.097707, 0.381809, 0.001324, 0.027932, 2.361600, -2.333600, -2.845200, -2.845200] test_list.append(flatplate) # Laminar cylinder (steady) @@ -174,7 +174,7 @@ def main(): cylinder.cfg_dir = "navierstokes/cylinder" cylinder.cfg_file = "lam_cylinder.cfg" cylinder.test_iter = 25 - cylinder.test_vals = [-8.363068, -2.882163, -0.017777, 1.607222, -0.010064] + cylinder.test_vals = [-8.363995, -2.882536, -0.017780, 1.607979, -0.010080] test_list.append(cylinder) # Laminar cylinder (low Mach correction) @@ -190,7 +190,7 @@ def main(): poiseuille.cfg_dir = "navierstokes/poiseuille" poiseuille.cfg_file = "lam_poiseuille.cfg" poiseuille.test_iter = 10 - poiseuille.test_vals = [-5.050732, 0.648355, 0.012273, 13.643219, -2.047100] + poiseuille.test_vals = [-5.050753, 0.648333, 0.012273, 13.643141, -2.114700] test_list.append(poiseuille) # 2D Poiseuille flow (inlet profile file) @@ -242,7 +242,7 @@ 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 = [-4.156553, -6.736064, -0.176184, 0.057478] + turb_flatplate.test_vals = [-4.312826, -6.736053, -0.187467, 0.057454] test_list.append(turb_flatplate) # FLAT PLATE, WALL FUNCTIONS, COMPRESSIBLE SST @@ -250,7 +250,7 @@ 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 = [-4.177397, -1.880811, -1.943377, 1.263787, -1.254740, 1.538892, 10.000000, -2.097623, 0.074673, 0.002932] + turb_wallfunction_flatplate_sst.test_vals = [-4.394471, -1.877558, -1.960378, 0.983694, -1.255671, 1.566842, 10.000000, -1.763190, 0.034806, 0.002921] test_list.append(turb_wallfunction_flatplate_sst) # FLAT PLATE, WALL FUNCTIONS, COMPRESSIBLE SA @@ -258,7 +258,7 @@ def main(): 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 = [-4.414833, -2.031596, -2.120806, 1.007586, -5.386444, 10.000000, -1.635112, 0.068983, 0.002640] + turb_wallfunction_flatplate_sa.test_vals = [-4.460537, -2.033605, -2.117564, 0.889626, -5.381903, 10.000000, -1.517487, 0.034212, 0.002636] test_list.append(turb_wallfunction_flatplate_sa) # ONERA M6 Wing @@ -266,7 +266,7 @@ def main(): turb_oneram6.cfg_dir = "rans/oneram6" turb_oneram6.cfg_file = "turb_ONERAM6.cfg" turb_oneram6.test_iter = 10 - turb_oneram6.test_vals = [-2.392867, -6.689823, 0.230746, 0.158811, -33786.000000] + turb_oneram6.test_vals = [-2.408533, -6.662837, 0.238334, 0.158910, -52718] turb_oneram6.timeout = 3200 test_list.append(turb_oneram6) @@ -294,7 +294,7 @@ 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 = [-7.690803, -10.049843, -3.414020, 1.049314, 0.019686, -2.207421, -45.199000] + turb_naca0012_sst_2003m.test_vals = [-7.688960, -10.046264, -3.405925, 1.049319, 0.019785, -2.214947, -45.588000] turb_naca0012_sst_2003m.timeout = 3200 test_list.append(turb_naca0012_sst_2003m) @@ -313,7 +313,7 @@ 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 = [-5.206797, -10.023481, -1.616002, 1.021528, 0.040220, -3.480532] + turb_naca0012_sst_fixedvalues.test_vals = [-5.206694, -10.016428, -1.616043, 1.021479, 0.040333, -3.478142] turb_naca0012_sst_fixedvalues.timeout = 3200 test_list.append(turb_naca0012_sst_fixedvalues) @@ -322,7 +322,7 @@ def main(): propeller.cfg_dir = "rans/propeller" propeller.cfg_file = "propeller.cfg" propeller.test_iter = 10 - propeller.test_vals = [-3.389575, -8.409251, 0.000048, 0.056329] + propeller.test_vals = [-3.389724, -8.409223, 0.000048, 0.056344] propeller.timeout = 3200 test_list.append(propeller) @@ -677,8 +677,7 @@ 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 = [-4.986094, 1.137009, 0.378604, -0.083526] - turb_naca0012_1c.test_vals_aarch64 = [-4.986054, 1.137073, 0.378618, -0.083513] + turb_naca0012_1c.test_vals = [-4.992120, 1.134926, 0.356004, -0.089085] test_list.append(turb_naca0012_1c) # NACA0012 2c @@ -686,8 +685,7 @@ 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 = [-5.483291, 0.968701, 0.258168, -0.114217] - turb_naca0012_2c.test_vals_aarch64 = [-5.483307, 0.968694, 0.258049, -0.114260] #last 4 columns + turb_naca0012_2c.test_vals = [-5.485136, 0.968075, 0.273236, -0.110320] test_list.append(turb_naca0012_2c) # NACA0012 3c @@ -695,7 +693,7 @@ def main(): 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 = [-5.584299, 0.931258, 0.251298, -0.114232] + turb_naca0012_3c.test_vals = [-5.584305, 0.931248, 0.250749, -0.113574] test_list.append(turb_naca0012_3c) # NACA0012 p1c1 @@ -703,8 +701,7 @@ def main(): 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 = [-5.127497, 1.077175, 0.546823, -0.023191] - turb_naca0012_p1c1.test_vals_aarch64 = [-5.127510, 1.077107, 0.546893, -0.023166] #last 4 columns + turb_naca0012_p1c1.test_vals = [-5.120263, 1.074826, 0.294764, -0.109420] test_list.append(turb_naca0012_p1c1) # NACA0012 p1c2 @@ -712,8 +709,7 @@ 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 = [-5.554412, 0.943562, 0.322803, -0.095946] - turb_naca0012_p1c2.test_vals_aarch64 = [-5.554381, 0.943577, 0.322676, -0.095989] #last 4 columns + turb_naca0012_p1c2.test_vals = [-5.549132, 0.945637, 0.252403, -0.117491] test_list.append(turb_naca0012_p1c2) ###################################### @@ -753,7 +749,7 @@ def main(): cavity.cfg_dir = "moving_wall/cavity" cavity.cfg_file = "lam_cavity.cfg" cavity.test_iter = 25 - cavity.test_vals = [-5.627868, -0.164405, 0.053283, 2.545817] + cavity.test_vals = [-5.627870, -0.164404, 0.054706, 2.545833] test_list.append(cavity) # Spinning cylinder @@ -761,7 +757,7 @@ 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 = [-7.892807, -2.467378, 1.702819, 1.669208] + spinning_cylinder.test_vals = [-7.894516, -2.469078, 1.703821, 1.670411] test_list.append(spinning_cylinder) ###################################### @@ -773,7 +769,7 @@ 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 = [-2.557884, -1.173573, 0.058052, 1.399794, 2.220411, 1.399748, 2.218612, -0.453340] + square_cylinder.test_vals = [-2.560840, -1.173495, 0.061186, 1.399403, 2.220585, 1.399351, 2.218790, -0.584750] square_cylinder.unsteady = True test_list.append(square_cylinder) @@ -876,8 +872,7 @@ 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 = [0.983751, 1.534480, -2.888520, 2.606773, -2.418421, 3.087187, 106380.000000, 106380.000000, 5.732500, 64.711000] - axial_stage2D.test_vals_aarch64 = [0.983751, 1.534480, -2.888520, 2.606773, -2.418421, 3.087187, 106380, 106380, 5.7325, 64.711] + axial_stage2D.test_vals = [0.987679, 1.532118, -2.888457, 2.606793, -2.418303, 3.087091, 106380.000000, 106380.000000, 5.732900, 64.728000] test_list.append(axial_stage2D) # 2D transonic stator restart @@ -915,8 +910,7 @@ 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, -0.202697, -13.249572] - uniform_flow.test_vals_aarch64 = [2.000000, 0.000000, -0.205134, -13.250720] #last 4 columns + uniform_flow.test_vals = [2.000000, 0.000000, -0.202598, -13.248144] uniform_flow.tol = 0.000001 uniform_flow.unsteady = True uniform_flow.multizone = True @@ -927,8 +921,7 @@ 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, 0.419778, 0.352185, 0.404395] - channel_2D.test_vals_aarch64 = [2.000000, 0.000000, 0.398053, 0.352788, 0.405474] #last 5 columns + channel_2D.test_vals = [2.000000, 0.000000, 0.417404, 0.350501, 0.401519] channel_2D.timeout = 100 channel_2D.unsteady = True channel_2D.multizone = True @@ -939,8 +932,7 @@ 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, 0.657678, 0.767752, 0.692208] - channel_3D.test_vals_aarch64 = [1.000000, 0.000000, 0.661408, 0.769902, 0.695663] #last 5 columns + channel_3D.test_vals = [1.000000, 0.000000, 0.656358, 0.766909, 0.690972] channel_3D.unsteady = True channel_3D.multizone = True test_list.append(channel_3D) @@ -950,7 +942,7 @@ def main(): pipe.cfg_dir = "sliding_interface/pipe" pipe.cfg_file = "pipe_NN.cfg" pipe.test_iter = 2 - pipe.test_vals = [0.481390, 0.648695, 0.982990, 1.018349] + pipe.test_vals = [0.477630, 0.641341, 0.983336, 1.018856] pipe.unsteady = True pipe.multizone = True test_list.append(pipe) @@ -970,7 +962,7 @@ 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, 1.207949, 1.036092] + supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.206774, 1.053444] supersonic_vortex_shedding.unsteady = True supersonic_vortex_shedding.multizone = True test_list.append(supersonic_vortex_shedding) @@ -1048,7 +1040,7 @@ def main(): fsi2d.cfg_dir = "fea_fsi/WallChannel_2d" fsi2d.cfg_file = "configFSI.cfg" fsi2d.test_iter = 4 - fsi2d.test_vals = [4.000000, 0.000000, -3.729228, -4.153949] + fsi2d.test_vals = [4.000000, 0.000000, -3.726050, -4.277800] fsi2d.multizone = True fsi2d.unsteady = True test_list.append(fsi2d) @@ -1058,7 +1050,7 @@ def main(): stat_fsi.cfg_dir = "fea_fsi/stat_fsi" stat_fsi.cfg_file = "config.cfg" stat_fsi.test_iter = 7 - stat_fsi.test_vals = [-3.345064, -4.996078, 0.000000, 7.000000] + stat_fsi.test_vals = [-3.343487, -4.993604, 0.000000, 7.000000] stat_fsi.multizone = True test_list.append(stat_fsi) @@ -1067,7 +1059,7 @@ def main(): stat_fsi_restart.cfg_dir = "fea_fsi/stat_fsi" stat_fsi_restart.cfg_file = "config_restart.cfg" stat_fsi_restart.test_iter = 1 - stat_fsi_restart.test_vals = [-3.404628, -4.288921, 0.000000, 27.000000] + stat_fsi_restart.test_vals = [-3.405333, -4.327317, 0.000000, 26.000000] stat_fsi_restart.multizone = True test_list.append(stat_fsi_restart) @@ -1076,8 +1068,7 @@ 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 = [-4.330444, -4.058003, 0.000000, 86.000000] - dyn_fsi.test_vals_aarch64 = [-4.355809, -4.060588, 0.000000, 86.000000] #last 4 columns + dyn_fsi.test_vals = [-4.330908, -4.153034, 0.000000, 86.000000] dyn_fsi.multizone = True dyn_fsi.unsteady = True test_list.append(dyn_fsi) @@ -1143,7 +1134,7 @@ def main(): mms_fvm_ns.cfg_dir = "mms/fvm_navierstokes" mms_fvm_ns.cfg_file = "lam_mms_roe.cfg" mms_fvm_ns.test_iter = 20 - mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000] + mms_fvm_ns.test_vals = [-2.808514, 2.152654, 0.000000, 0.000000] mms_fvm_ns.tol = 0.0001 test_list.append(mms_fvm_ns) @@ -1486,7 +1477,7 @@ def main(): opt_multiobj1surf_py.cfg_dir = "optimization_euler/multiobjective_wedge" opt_multiobj1surf_py.cfg_file = "inv_wedge_ROE_multiobj_1surf.cfg" opt_multiobj1surf_py.test_iter = 1 - opt_multiobj1surf_py.test_vals = [1.000000, 1.000000, 36.117740, 4.438036] + opt_multiobj1surf_py.test_vals = [1.000000, 1.000000, 36.139240, 4.307073] opt_multiobj1surf_py.command = TestCase.Command(exec = "shape_optimization.py", param = "-g CONTINUOUS_ADJOINT -f") opt_multiobj1surf_py.timeout = 1600 opt_multiobj1surf_py.tol = 0.00001 @@ -1499,7 +1490,7 @@ def main(): opt_2surf1obj_py.cfg_dir = "optimization_euler/multiobjective_wedge" opt_2surf1obj_py.cfg_file = "inv_wedge_ROE_2surf_1obj.cfg" opt_2surf1obj_py.test_iter = 1 - opt_2surf1obj_py.test_vals = [1.000000, 1.000000, 2.005219, 0.000369] + opt_2surf1obj_py.test_vals = [1.000000, 1.000000, 2.005099, 0.000358] opt_2surf1obj_py.command = TestCase.Command(exec = "shape_optimization.py", param = "-g CONTINUOUS_ADJOINT -f") opt_2surf1obj_py.timeout = 1600 opt_2surf1obj_py.tol = 0.00001 @@ -1516,7 +1507,7 @@ 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 = [-4.444941, -3.941038, 0.318998, 0.022365] + pywrapper_naca0012.test_vals = [-4.431325, -3.970055, 0.319205, 0.022299] pywrapper_naca0012.command = TestCase.Command(exec = "SU2_CFD.py", param = "-f") pywrapper_naca0012.timeout = 1600 pywrapper_naca0012.tol = 0.00001 @@ -1543,7 +1534,7 @@ 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 = [-2.557884, -1.173573, 0.058052, 1.399794, 2.220411, 1.399748, 2.218612, -0.453340] + pywrapper_square_cylinder.test_vals = [-2.560840, -1.173495, 0.061186, 1.399403, 2.220585, 1.399351, 2.218790, -0.584750] pywrapper_square_cylinder.command = TestCase.Command(exec = "SU2_CFD.py", param = "-f") pywrapper_square_cylinder.timeout = 1600 pywrapper_square_cylinder.tol = 0.00001 @@ -1571,7 +1562,7 @@ def main(): pywrapper_fsi2d.cfg_dir = "fea_fsi/WallChannel_2d" pywrapper_fsi2d.cfg_file = "configFSI.cfg" pywrapper_fsi2d.test_iter = 4 - pywrapper_fsi2d.test_vals = [4.000000, 0.000000, -3.729228, -4.153949] + pywrapper_fsi2d.test_vals = [4.000000, 0.000000, -3.726050, -4.277800] pywrapper_fsi2d.command = TestCase.Command(exec = "SU2_CFD.py", param = "--nZone 2 --fsi True -f") pywrapper_fsi2d.unsteady = True pywrapper_fsi2d.multizone = True @@ -1614,7 +1605,7 @@ def main(): pywrapper_custom_inlet.cfg_dir = "py_wrapper/custom_inlet" pywrapper_custom_inlet.cfg_file = "lam_flatplate.cfg" pywrapper_custom_inlet.test_iter = 20 - pywrapper_custom_inlet.test_vals = [-4.120494, -1.540195, -3.566114, 1.342509, -0.748827, 0.161349, -0.013214, 0.516000, -0.529220] + pywrapper_custom_inlet.test_vals = [-4.120585, -1.540325, -3.560392, 1.342419, -0.748768, 0.161248, -0.013208, 0.515780, -0.528990] pywrapper_custom_inlet.command = TestCase.Command(exec = "python", param = "run.py") pywrapper_custom_inlet.timeout = 1600 pywrapper_custom_inlet.tol = 0.0001