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revert some configs, fix regressions
1 parent 7ddc4e6 commit cd86b22

6 files changed

Lines changed: 14 additions & 14 deletions

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TestCases/ddes/flatplate/ddes_flatplate.cfg

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -227,4 +227,4 @@ SURFACE_ADJ_FILENAME= surface_adjoint
227227
OUTPUT_WRT_FREQ= 1000
228228
%
229229
% Screen output
230-
SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG, TOTAL_HEATFLUX)
230+
SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG, TOTAL_HEATFLUX)

TestCases/hybrid_regression.py

Lines changed: 2 additions & 2 deletions
Original file line numberDiff line numberDiff line change
@@ -254,8 +254,8 @@ def main():
254254
axi_rans_air_nozzle.cfg_dir = "axisymmetric_rans/air_nozzle"
255255
axi_rans_air_nozzle.cfg_file = "air_nozzle.cfg"
256256
axi_rans_air_nozzle.test_iter = 10
257-
axi_rans_air_nozzle.test_vals = [-12.093575, -6.630426, -8.798725, -2.399130, 0.0]
258-
axi_rans_air_nozzle.test_vals_aarch64 = [-12.093539, -6.630357, -8.798732, -2.399130, 0.0]
257+
axi_rans_air_nozzle.test_vals = [-12.093575, -6.630426, -8.798725, -2.399130, -1938.200000]
258+
axi_rans_air_nozzle.test_vals_aarch64 = [-12.093539, -6.630357, -8.798732, -2.399130, -1938.200000]
259259
test_list.append(axi_rans_air_nozzle)
260260

261261
#################################

TestCases/incomp_navierstokes/cylinder/incomp_cylinder.cfg

Lines changed: 1 addition & 0 deletions
Original file line numberDiff line numberDiff line change
@@ -183,3 +183,4 @@ OUTPUT_WRT_FREQ= 100
183183
%
184184
% Screen output fields
185185
SCREEN_OUTPUT= (INNER_ITER, RMS_PRESSURE, RMS_VELOCITY-X, LIFT, DRAG)
186+

TestCases/parallel_regression.py

Lines changed: 5 additions & 5 deletions
Original file line numberDiff line numberDiff line change
@@ -462,7 +462,7 @@ def main():
462462
axi_rans_air_nozzle.cfg_dir = "axisymmetric_rans/air_nozzle"
463463
axi_rans_air_nozzle.cfg_file = "air_nozzle.cfg"
464464
axi_rans_air_nozzle.test_iter = 10
465-
axi_rans_air_nozzle.test_vals = [-12.096377, -6.636625, -8.786639, -2.399099, 0.0]
465+
axi_rans_air_nozzle.test_vals = [-12.096377, -6.636625, -8.786639, -2.399099, -1938.200000]
466466
axi_rans_air_nozzle.su2_exec = "mpirun -n 2 SU2_CFD"
467467
axi_rans_air_nozzle.timeout = 1600
468468
axi_rans_air_nozzle.tol = 0.0001
@@ -1044,7 +1044,7 @@ def main():
10441044
square_cylinder.cfg_dir = "unsteady/square_cylinder"
10451045
square_cylinder.cfg_file = "turb_square.cfg"
10461046
square_cylinder.test_iter = 3
1047-
square_cylinder.test_vals = [-1.406732, 0.036325, 1.399116, 2.199754, 1.399116, 2.199754, -0.399740]
1047+
square_cylinder.test_vals = [-1.162664, 0.066378, 1.399789, 2.220404, 1.399743, 2.218605, -0.453170]
10481048
square_cylinder.su2_exec = "parallel_computation.py -f"
10491049
square_cylinder.timeout = 1600
10501050
square_cylinder.tol = 0.00001
@@ -1080,7 +1080,7 @@ def main():
10801080
ddes_flatplate.cfg_dir = "ddes/flatplate"
10811081
ddes_flatplate.cfg_file = "ddes_flatplate.cfg"
10821082
ddes_flatplate.test_iter = 10
1083-
ddes_flatplate.test_vals = [-3.826301, -6.378282, -0.013762, 0.106606, -11664.000000]
1083+
ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783, -618.160000]
10841084
ddes_flatplate.su2_exec = "parallel_computation.py -f"
10851085
ddes_flatplate.timeout = 1600
10861086
ddes_flatplate.tol = 0.00001
@@ -1409,7 +1409,7 @@ def main():
14091409
p1rad.cfg_file = "configp1.cfg"
14101410
p1rad.new_output= True
14111411
p1rad.test_iter = 100
1412-
p1rad.test_vals = [-7.743666, -7.921411, -2.111848, 0.098302, 0.0] #last 4 columns
1412+
p1rad.test_vals = [-7.743666, -7.921411, -2.111848, 0.098302, -45.023000]
14131413
p1rad.su2_exec = "mpirun -n 2 SU2_CFD"
14141414
p1rad.timeout = 1600
14151415
p1rad.tol = 0.00001
@@ -1516,7 +1516,7 @@ def main():
15161516
pywrapper_square_cylinder.cfg_dir = "unsteady/square_cylinder"
15171517
pywrapper_square_cylinder.cfg_file = "turb_square.cfg"
15181518
pywrapper_square_cylinder.test_iter = 3
1519-
pywrapper_square_cylinder.test_vals = [-1.162664, 0.066378, 1.399789, 2.220404, 1.399743, 2.218605, -0.399740]
1519+
pywrapper_square_cylinder.test_vals = [-1.162664, 0.066378, 1.399789, 2.220404, 1.399743, 2.218605, -0.453170]
15201520
pywrapper_square_cylinder.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
15211521
pywrapper_square_cylinder.timeout = 1600
15221522
pywrapper_square_cylinder.tol = 0.00001

TestCases/serial_regression.py

Lines changed: 4 additions & 4 deletions
Original file line numberDiff line numberDiff line change
@@ -434,7 +434,7 @@ def main():
434434
axi_rans_air_nozzle.cfg_dir = "axisymmetric_rans/air_nozzle"
435435
axi_rans_air_nozzle.cfg_file = "air_nozzle.cfg"
436436
axi_rans_air_nozzle.test_iter = 10
437-
axi_rans_air_nozzle.test_vals = [ -12.092891, -6.630495, -8.784840, -2.399099, 0.0]
437+
axi_rans_air_nozzle.test_vals = [-12.092891, -6.630495, -8.784840, -2.399099, -1938.200000]
438438
axi_rans_air_nozzle.su2_exec = "SU2_CFD"
439439
axi_rans_air_nozzle.timeout = 1600
440440
axi_rans_air_nozzle.tol = 0.0001
@@ -1028,7 +1028,7 @@ def main():
10281028
square_cylinder.cfg_dir = "unsteady/square_cylinder"
10291029
square_cylinder.cfg_file = "turb_square.cfg"
10301030
square_cylinder.test_iter = 3
1031-
square_cylinder.test_vals = [-2.926876, -1.406729, 0.036316, 1.399116, 2.199756, 1.399116, 2.199756, -0.399760]
1031+
square_cylinder.test_vals = [-2.557893, -1.162560, 0.066414, 1.399788, 2.220411, 1.399743, 2.218612, -0.453170]
10321032
square_cylinder.su2_exec = "SU2_CFD"
10331033
square_cylinder.timeout = 1600
10341034
square_cylinder.tol = 0.00001
@@ -1067,7 +1067,7 @@ def main():
10671067
ddes_flatplate.cfg_dir = "ddes/flatplate"
10681068
ddes_flatplate.cfg_file = "ddes_flatplate.cfg"
10691069
ddes_flatplate.test_iter = 10
1070-
ddes_flatplate.test_vals = [-3.826301, -6.378282, -0.013762, 0.106606, -11664.000000]
1070+
ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783, -618.160000]
10711071
ddes_flatplate.su2_exec = "SU2_CFD"
10721072
ddes_flatplate.timeout = 1600
10731073
ddes_flatplate.tol = 0.00001
@@ -1457,7 +1457,7 @@ def main():
14571457
p1rad.cfg_file = "configp1.cfg"
14581458
p1rad.new_output= True
14591459
p1rad.test_iter = 100
1460-
p1rad.test_vals = [-7.751309, -7.923059, -2.119084, 0.091733, 0.0] #last 4 columns
1460+
p1rad.test_vals = [-7.751309, -7.923059, -2.119084, 0.091733, -44.537000]
14611461
p1rad.su2_exec = "SU2_CFD"
14621462
p1rad.timeout = 1600
14631463
p1rad.tol = 0.00001

TestCases/unsteady/square_cylinder/turb_square.cfg

Lines changed: 1 addition & 2 deletions
Original file line numberDiff line numberDiff line change
@@ -252,8 +252,7 @@ SURFACE_ADJ_FILENAME= surface_adjoint
252252
% Writing solution file frequency for physical time steps (dual time)
253253
OUTPUT_WRT_FREQ= 1
254254
%
255-
%
256255
% Screen output
257-
SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, TAVG_LIFT, TAVG_DRAG, TOTAL_HEATFLUX)
256+
SCREEN_OUTPUT= (TIME_ITER, INNER_ITER, RMS_DENSITY, RMS_TKE, RMS_DISSIPATION, LIFT, DRAG, TAVG_LIFT, TAVG_DRAG, TOTAL_HEATFLUX)
258257
%
259258
OUTPUT_FILES= (RESTART_ASCII)

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