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‎TestCases/hybrid_regression.py‎

Lines changed: 10 additions & 10 deletions
Original file line numberDiff line numberDiff line change
@@ -207,17 +207,17 @@ def main():
207207
turb_naca0012_sst.cfg_dir = "rans/naca0012"
208208
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
209209
turb_naca0012_sst.test_iter = 10
210-
turb_naca0012_sst.test_vals = [-11.418415, -12.801780, -5.864804, 1.049990, 0.019163, -1.669899, -38.695000]
211-
turb_naca0012_sst.test_vals_aarch64 = [-11.450473, -12.797872, -5.863655, 1.049989, 0.019163, -1.856266, -38.694000]
210+
turb_naca0012_sst.test_vals = [-12.216989, -14.439370, -7.108639, 1.050109, 0.019148, -1.483537, -38.510000]
211+
turb_naca0012_sst.test_vals_aarch64 = [-12.216989, -14.439370, -7.108639, 1.050109, 0.019148, -1.483537, -38.510000]
212212
test_list.append(turb_naca0012_sst)
213213

214214
# NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
215215
turb_naca0012_sst_sust = TestCase('turb_naca0012_sst_sust')
216216
turb_naca0012_sst_sust.cfg_dir = "rans/naca0012"
217217
turb_naca0012_sst_sust.cfg_file = "turb_NACA0012_sst_sust.cfg"
218218
turb_naca0012_sst_sust.test_iter = 10
219-
turb_naca0012_sst_sust.test_vals = [-11.361657, -12.642245, -5.747099, 1.005234, 0.019017, -1.573783]
220-
turb_naca0012_sst_sust.test_vals_aarch64 = [-11.367052, -12.640670, -5.746919, 1.005233, 0.019017, -1.913907]
219+
turb_naca0012_sst_sust.test_vals = [-12.148204, -14.755890, -6.342986, 1.001189, 0.019384, -1.432333]
220+
turb_naca0012_sst_sust.test_vals_aarch64 = [-12.148204, -14.755890, -6.342986, 1.001189, 0.019384, -1.432333]
221221
test_list.append(turb_naca0012_sst_sust)
222222

223223
# NACA0012 (SST, fixed values for turbulence quantities)
@@ -254,8 +254,8 @@ def main():
254254
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
255255
axi_rans_air_nozzle_restart.cfg_file = "air_nozzle_restart.cfg"
256256
axi_rans_air_nozzle_restart.test_iter = 10
257-
axi_rans_air_nozzle_restart.test_vals = [-12.085749, -7.439410, -8.772091, -4.045091, -1924.800000]
258-
axi_rans_air_nozzle_restart.test_vals_aarch64 = [-12.093539, -6.630357, -8.798732, -2.399130, -1938.200000]
257+
axi_rans_air_nozzle_restart.test_vals = [-12.060634, -6.992273, -8.808757, -4.097753, -2019.800000]
258+
axi_rans_air_nozzle_restart.test_vals_aarch64 = [-12.060634, -6.992273, -8.808757, -4.097753, -2019.800000]
259259
test_list.append(axi_rans_air_nozzle_restart)
260260

261261
#################################
@@ -470,7 +470,7 @@ def main():
470470
sine_gust.test_vals = [-1.977520, 3.481804, -0.012402, -0.007454]
471471
sine_gust.unsteady = True
472472
test_list.append(sine_gust)
473-
473+
474474
# Cosine gust in z-direction
475475
cosine_gust = TestCase('cosine_gust_zdir')
476476
cosine_gust.cfg_dir = "gust"
@@ -479,7 +479,7 @@ def main():
479479
cosine_gust.test_vals = [-2.418813, 0.004650, -0.001878, -0.000637, -0.000271]
480480
cosine_gust.unsteady = True
481481
test_list.append(cosine_gust)
482-
482+
483483
# Gust with mesh deformation
484484
gust_mesh_defo = TestCase('gust_with_mesh_deformation')
485485
gust_mesh_defo.cfg_dir = "gust"
@@ -557,7 +557,7 @@ def main():
557557
Jones_tc_restart.cfg_dir = "turbomachinery/APU_turbocharger"
558558
Jones_tc_restart.cfg_file = "Jones_restart.cfg"
559559
Jones_tc_restart.test_iter = 5
560-
Jones_tc_restart.test_vals = [-6.986581, -3.096834, -14.849548, -9.102930, -11.787851, -6.266207, 73266, 73266]
560+
Jones_tc_restart.test_vals = [-6.604542, -2.792279, -14.328530, -8.769313, -11.371439, -5.845633, 73273.000000, 73273.000000]
561561
test_list.append(Jones_tc_restart)
562562

563563
# 2D axial stage
@@ -769,7 +769,7 @@ def main():
769769
pywrapper_translating_naca0012.test_file = "forces_0.csv"
770770
pywrapper_translating_naca0012.enabled_on_cpu_arch = ["x86_64"]
771771
file_diff_list.append(pywrapper_translating_naca0012)
772-
772+
773773
# NACA0012 with updated moving frame
774774
pywrapper_updated_moving_frame_naca0012 = TestCase('pywrapper_updated_moving_frame_naca0012')
775775
pywrapper_updated_moving_frame_naca0012.cfg_dir = "py_wrapper/updated_moving_frame_NACA12"

‎TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/of_grad_findiff.csv.ref‎

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -1,2 +1,2 @@
11
"VARIABLE" , "AVG_DENSITY[0]", "AVG_ENTHALPY[0]", "AVG_NORMALVEL[0]", "DRAG[0]" , "EFFICIENCY[0]" , "FORCE_X[0]" , "FORCE_Y[0]" , "FORCE_Z[0]" , "LIFT[0]" , "MOMENT_X[0]" , "MOMENT_Y[0]" , "MOMENT_Z[0]" , "SIDEFORCE[0]" , "SURFACE_MACH[0]", "SURFACE_MASSFLOW[0]", "SURFACE_MOM_DISTORTION[0]", "SURFACE_PRESSURE_DROP[0]", "SURFACE_SECONDARY[0]", "SURFACE_SECOND_OVER_UNIFORM[0]", "SURFACE_STATIC_PRESSURE[0]", "SURFACE_STATIC_TEMPERATURE[0]", "SURFACE_TOTAL_PRESSURE[0]", "SURFACE_TOTAL_TEMPERATURE[0]", "SURFACE_UNIFORMITY[0]", "AVG_TEMPERATURE[1]", "MAXIMUM_HEATFLUX[1]", "TOTAL_HEATFLUX[1]", "FINDIFF_STEP"
2-
0 , 0.0 , -100000.01639127731, -1.1103000000496327e-08, 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , -0.0399999991462785, 3.3309999998872306e-08, -2.1099999997220564 , 0.0 , 2.1799999999627673 , 3.8000000007754053 , 319.9999980552093 , -39.999997625272954 , 318.0000007318995 , -39.999997625272954 , -1.400000004814217 , -139.99999737279722, 0.0 , -540.0000077315781, 1e-08
2+
0 , 0.0 , -199999.9862164259, -5.551100000002363e-08, 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , -0.02000000026702864, 5.550999999230055e-08, -0.6560000001543109 , 0.0 , 0.6520000012111282 , 1.1399999999550658 , 319.9999980552093 , -39.999997625272954 , 260.999999568412 , -39.999997625272954 , -0.4999999969612645 , -269.99999818144715, 0.0 , -560.0000008598727, 1e-08

‎TestCases/parallel_regression.py‎

Lines changed: 9 additions & 9 deletions
Original file line numberDiff line numberDiff line change
@@ -413,7 +413,7 @@ def main():
413413
turb_naca0012_sst.cfg_dir = "rans/naca0012"
414414
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
415415
turb_naca0012_sst.test_iter = 10
416-
turb_naca0012_sst.test_vals = [-11.422619, -12.803419, -5.867375, 1.049989, 0.019163, -1.827695, -38.695000]
416+
turb_naca0012_sst.test_vals = [-12.219694, -14.440925, -7.107551, 1.050109, 0.019148, -1.601287, -38.510000]
417417
turb_naca0012_sst.timeout = 3200
418418
test_list.append(turb_naca0012_sst)
419419

@@ -422,7 +422,7 @@ def main():
422422
turb_naca0012_sst_sust.cfg_dir = "rans/naca0012"
423423
turb_naca0012_sst_sust.cfg_file = "turb_NACA0012_sst_sust.cfg"
424424
turb_naca0012_sst_sust.test_iter = 10
425-
turb_naca0012_sst_sust.test_vals = [-11.366100, -12.643576, -5.749377, 1.005234, 0.019017, -1.818746]
425+
turb_naca0012_sst_sust.test_vals = [-12.148637, -14.756583, -6.342201, 1.001189, 0.019384, -1.579100]
426426
turb_naca0012_sst_sust.timeout = 3200
427427
test_list.append(turb_naca0012_sst_sust)
428428

@@ -431,7 +431,7 @@ def main():
431431
turb_naca0012_sst_2003_Vm.cfg_dir = "rans/naca0012"
432432
turb_naca0012_sst_2003_Vm.cfg_file = "turb_NACA0012_sst_2003-Vm.cfg"
433433
turb_naca0012_sst_2003_Vm.test_iter = 10
434-
turb_naca0012_sst_2003_Vm.test_vals = [-7.672926, -10.025010, -3.365892, 1.048735, 0.019723, -2.052543]
434+
turb_naca0012_sst_2003_Vm.test_vals = [-7.664806, -10.014760, -3.358584, 1.048643, 0.019718, -2.067883]
435435
turb_naca0012_sst_2003_Vm.timeout = 3200
436436
test_list.append(turb_naca0012_sst_2003_Vm)
437437

@@ -440,7 +440,7 @@ def main():
440440
turb_naca0012_sst_1994_KLm.cfg_dir = "rans/naca0012"
441441
turb_naca0012_sst_1994_KLm.cfg_file = "turb_NACA0012_sst_1994-KLm.cfg"
442442
turb_naca0012_sst_1994_KLm.test_iter = 10
443-
turb_naca0012_sst_1994_KLm.test_vals = [-8.616539, -10.868753, -4.060879, 1.049473, 0.019192, -1.867965]
443+
turb_naca0012_sst_1994_KLm.test_vals = [-8.570837, -10.805211, -3.997146, 1.049397, 0.019183, -1.805750]
444444
turb_naca0012_sst_1994_KLm.timeout = 3200
445445
test_list.append(turb_naca0012_sst_1994_KLm)
446446

@@ -481,7 +481,7 @@ def main():
481481
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
482482
axi_rans_air_nozzle_restart.cfg_file = "air_nozzle_restart.cfg"
483483
axi_rans_air_nozzle_restart.test_iter = 10
484-
axi_rans_air_nozzle_restart.test_vals = [-12.089268, -7.493381, -8.716391, -4.021218, -1924.800000]
484+
axi_rans_air_nozzle_restart.test_vals = [-12.063597, -7.006585, -8.702557, -4.039824, -2019.0]
485485
axi_rans_air_nozzle_restart.tol = 0.0001
486486
test_list.append(axi_rans_air_nozzle_restart)
487487

@@ -1015,7 +1015,7 @@ def main():
10151015
Jones_tc_restart.cfg_dir = "turbomachinery/APU_turbocharger"
10161016
Jones_tc_restart.cfg_file = "Jones_restart.cfg"
10171017
Jones_tc_restart.test_iter = 5
1018-
Jones_tc_restart.test_vals = [-6.986563, -3.096834, -14.849532, -9.102914, -11.787851, -6.266208, 7.3266e+04, 7.3266e+04]
1018+
Jones_tc_restart.test_vals = [-6.604542, -2.792281, -14.328530, -8.769313, -11.371439, -5.845632, 73273, 73273]
10191019
test_list.append(Jones_tc_restart)
10201020

10211021
# 2D axial stage
@@ -1256,8 +1256,8 @@ def main():
12561256
sp_pinArray_3d_cht_mf_hf_tp.cfg_dir = "incomp_navierstokes/streamwise_periodic/chtPinArray_3d"
12571257
sp_pinArray_3d_cht_mf_hf_tp.cfg_file = "configMaster.cfg"
12581258
sp_pinArray_3d_cht_mf_hf_tp.test_iter = 30
1259-
sp_pinArray_3d_cht_mf_hf_tp.test_vals = [-3.773085, -4.220555, -4.811282, -0.009675, 99.879858, 419.200000, 0.000000]
1260-
sp_pinArray_3d_cht_mf_hf_tp.test_vals_aarch64 = [-13.400623, -7.476945, -7.025285, -0.009675, 99.879812, 419.200000, 0.0]
1259+
sp_pinArray_3d_cht_mf_hf_tp.test_vals = [-5.109072, -5.409931, -6.807748, -0.009675, 104.655093, 4.1921e+02, 0.0]
1260+
sp_pinArray_3d_cht_mf_hf_tp.test_vals_aarch64 = [-5.109072, -5.409931, -6.807748, -0.009675, 104.655093, 4.1921e+02, 0.0]
12611261
sp_pinArray_3d_cht_mf_hf_tp.multizone = True
12621262
test_list.append(sp_pinArray_3d_cht_mf_hf_tp)
12631263

@@ -1279,7 +1279,7 @@ def main():
12791279
pywrapper_turb_naca0012_sst.cfg_dir = "rans/naca0012"
12801280
pywrapper_turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
12811281
pywrapper_turb_naca0012_sst.test_iter = 10
1282-
pywrapper_turb_naca0012_sst.test_vals = [-11.422619, -12.803419, -5.867375, 1.049989, 0.019163, -1.827695, -38.695000]
1282+
pywrapper_turb_naca0012_sst.test_vals = [-12.219694, -14.440925, -7.107551, 1.050109, 0.019148, -1.601287, -38.510000]
12831283
pywrapper_turb_naca0012_sst.command = TestCase.Command("mpirun -np 2", "SU2_CFD.py", "--parallel -f")
12841284
pywrapper_turb_naca0012_sst.timeout = 3200
12851285
test_list.append(pywrapper_turb_naca0012_sst)

‎TestCases/serial_regression.py‎

Lines changed: 7 additions & 7 deletions
Original file line numberDiff line numberDiff line change
@@ -279,8 +279,8 @@ def main():
279279
turb_naca0012_sst.cfg_dir = "rans/naca0012"
280280
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
281281
turb_naca0012_sst.test_iter = 10
282-
turb_naca0012_sst.test_vals = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
283-
turb_naca0012_sst.test_vals_aarch64 = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
282+
turb_naca0012_sst.test_vals = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
283+
turb_naca0012_sst.test_vals_aarch64 = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
284284
turb_naca0012_sst.timeout = 3200
285285
test_list.append(turb_naca0012_sst)
286286

@@ -289,7 +289,7 @@ def main():
289289
turb_naca0012_sst_2003m.cfg_dir = "rans/naca0012"
290290
turb_naca0012_sst_2003m.cfg_file = "turb_NACA0012_sst_2003m.cfg"
291291
turb_naca0012_sst_2003m.test_iter = 10
292-
turb_naca0012_sst_2003m.test_vals = [-7.698427, -10.060122, -3.421605, 1.049413, 0.019691, -2.193374, -45.178000]
292+
turb_naca0012_sst_2003m.test_vals = [-7.690803, -10.049843, -3.414020, 1.049314, 0.019686, -2.207421, -45.199000]
293293
turb_naca0012_sst_2003m.timeout = 3200
294294
test_list.append(turb_naca0012_sst_2003m)
295295

@@ -298,7 +298,7 @@ def main():
298298
turb_naca0012_sst_sust_restart.cfg_dir = "rans/naca0012"
299299
turb_naca0012_sst_sust_restart.cfg_file = "turb_NACA0012_sst_sust.cfg"
300300
turb_naca0012_sst_sust_restart.test_iter = 10
301-
turb_naca0012_sst_sust_restart.test_vals = [-12.006877, -14.685697, -6.270559, 1.001189, 0.019384, -1.435246]
301+
turb_naca0012_sst_sust_restart.test_vals = [-12.153015, -14.756601, -6.342509, 1.001189, 0.019384, -1.820009]
302302
turb_naca0012_sst_sust_restart.timeout = 3200
303303
test_list.append(turb_naca0012_sst_sust_restart)
304304

@@ -329,7 +329,7 @@ def main():
329329
axi_rans_air_nozzle_restart.cfg_dir = "axisymmetric_rans/air_nozzle"
330330
axi_rans_air_nozzle_restart.cfg_file = "air_nozzle_restart.cfg"
331331
axi_rans_air_nozzle_restart.test_iter = 10
332-
axi_rans_air_nozzle_restart.test_vals = [-12.003752, -6.926896, -8.627670, -4.003588, -2.0198e+03]
332+
axi_rans_air_nozzle_restart.test_vals = [-12.063377, -7.005051, -8.705733, -4.036815, -2019.8]
333333
axi_rans_air_nozzle_restart.tol = 0.0001
334334
test_list.append(axi_rans_air_nozzle_restart)
335335

@@ -1496,8 +1496,8 @@ def main():
14961496
pywrapper_turb_naca0012_sst.cfg_dir = "rans/naca0012"
14971497
pywrapper_turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
14981498
pywrapper_turb_naca0012_sst.test_iter = 10
1499-
pywrapper_turb_naca0012_sst.test_vals = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
1500-
pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.007177, -14.272504, -6.994514, 1.050109, 0.019148, -1.455402, -3.8510e+01]
1499+
pywrapper_turb_naca0012_sst.test_vals = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
1500+
pywrapper_turb_naca0012_sst.test_vals_aarch64 = [-12.213755, -14.439873, -7.108062, 1.050109, 0.019148, -1.875539, -38.510000]
15011501
pywrapper_turb_naca0012_sst.command = TestCase.Command(exec = "SU2_CFD.py", param = "-f")
15021502
pywrapper_turb_naca0012_sst.timeout = 3200
15031503
pywrapper_turb_naca0012_sst.tol = 0.00001

‎TestCases/turbomachinery/transonic_stator_2D/transonic_stator_restart.cfg‎

Lines changed: 1 addition & 0 deletions
Original file line numberDiff line numberDiff line change
@@ -13,6 +13,7 @@
1313
%
1414
SOLVER= RANS
1515
KIND_TURB_MODEL= SST
16+
SST_OPTIONS= V1994m
1617
MATH_PROBLEM= DIRECT
1718
RESTART_SOL= YES
1819
DISCARD_INFILES= NO

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