@@ -109,26 +109,26 @@ def main():
109109 cylinder .cfg_dir = "navierstokes/cylinder"
110110 cylinder .cfg_file = "lam_cylinder.cfg"
111111 cylinder .test_iter = 25
112- cylinder .test_vals = [- 6.765429 , - 1.297425 , 0.019571 , 0.310232 ]
113- cylinder .test_vals_aarch64 = [- 6.765429 , - 1.297425 , 0.019571 , 0.310231 ]
112+ cylinder .test_vals = [- 6.765429 , - 1.297425 , 0.019571 , 0.310232 , 0.123270 ]
113+ cylinder .test_vals_aarch64 = [- 6.765429 , - 1.297425 , 0.019571 , 0.310231 , 0.123270 ]
114114 test_list .append (cylinder )
115115
116116 # Laminar cylinder (low Mach correction)
117117 cylinder_lowmach = TestCase ('cylinder_lowmach' )
118118 cylinder_lowmach .cfg_dir = "navierstokes/cylinder"
119119 cylinder_lowmach .cfg_file = "cylinder_lowmach.cfg"
120120 cylinder_lowmach .test_iter = 25
121- cylinder_lowmach .test_vals = [- 6.850130 , - 1.388096 , - 0.056036 , 108.140811 ]
122- cylinder_lowmach .test_vals_aarch64 = [- 6.850130 , - 1.388096 , - 0.056036 , 108.140813 ]
121+ cylinder_lowmach .test_vals = [- 6.850130 , - 1.388096 , - 0.056036 , 108.140811 , 0.007988 ]
122+ cylinder_lowmach .test_vals_aarch64 = [- 6.850130 , - 1.388096 , - 0.056036 , 108.140813 , 0.007988 ]
123123 test_list .append (cylinder_lowmach )
124124
125125 # 2D Poiseuille flow (body force driven with periodic inlet / outlet)
126126 poiseuille = TestCase ('poiseuille' )
127127 poiseuille .cfg_dir = "navierstokes/poiseuille"
128128 poiseuille .cfg_file = "lam_poiseuille.cfg"
129129 poiseuille .test_iter = 10
130- poiseuille .test_vals = [- 5.048282 , 0.650814 , 0.008714 , 13.677678 ]
131- poiseuille .test_vals_aarch64 = [- 5.048282 , 0.650814 , 0.008713 , 13.677691 ]
130+ poiseuille .test_vals = [- 5.048282 , 0.650814 , 0.008714 , 13.677678 , - 2.054800 ]
131+ poiseuille .test_vals_aarch64 = [- 5.048282 , 0.650814 , 0.008713 , 13.677691 , - 2.054800 ]
132132 test_list .append (poiseuille )
133133
134134 # 2D Poiseuille flow (inlet profile file)
@@ -158,15 +158,15 @@ def main():
158158 rae2822_sa .cfg_dir = "rans/rae2822"
159159 rae2822_sa .cfg_file = "turb_SA_RAE2822.cfg"
160160 rae2822_sa .test_iter = 20
161- rae2822_sa .test_vals = [- 2.020123 , - 5.269330 , 0.807147 , 0.060499 ]
161+ rae2822_sa .test_vals = [- 2.020123 , - 5.269330 , 0.807147 , 0.060499 , - 80603.000000 ]
162162 test_list .append (rae2822_sa )
163163
164164 # RAE2822 SST
165165 rae2822_sst = TestCase ('rae2822_sst' )
166166 rae2822_sst .cfg_dir = "rans/rae2822"
167167 rae2822_sst .cfg_file = "turb_SST_RAE2822.cfg"
168168 rae2822_sst .test_iter = 20
169- rae2822_sst .test_vals = [- 0.510635 , 4.871104 , 0.811904 , 0.061614 ]
169+ rae2822_sst .test_vals = [- 0.510635 , 4.871104 , 0.811904 , 0.061614 , - 82395.000000 ]
170170 test_list .append (rae2822_sst )
171171
172172 # RAE2822 SST_SUST
@@ -190,25 +190,25 @@ def main():
190190 turb_oneram6 .cfg_dir = "rans/oneram6"
191191 turb_oneram6 .cfg_file = "turb_ONERAM6.cfg"
192192 turb_oneram6 .test_iter = 10
193- turb_oneram6 .test_vals = [- 2.388836 , - 6.689414 , 0.230320 , 0.157640 ]
193+ turb_oneram6 .test_vals = [- 2.388836 , - 6.689414 , 0.230320 , 0.157640 , - 32539.000000 ]
194194 test_list .append (turb_oneram6 )
195195
196196 # NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
197197 turb_naca0012_sa = TestCase ('turb_naca0012_sa' )
198198 turb_naca0012_sa .cfg_dir = "rans/naca0012"
199199 turb_naca0012_sa .cfg_file = "turb_NACA0012_sa.cfg"
200200 turb_naca0012_sa .test_iter = 10
201- turb_naca0012_sa .test_vals = [- 8.627052 , - 10.377936 , 1.064491 , 0.019710 , 20.000000 , - 1.763095 , 20.000000 , - 4.794176 ]
202- turb_naca0012_sa .test_vals_aarch64 = [- 8.627052 , - 10.377936 , 1.064491 , 0.019710 , 20.000000 , - 1.763093 , 20.000000 , - 4.794073 ]
201+ turb_naca0012_sa .test_vals = [- 8.627052 , - 10.377936 , 1.064491 , 0.019710 , 20.000000 , - 1.763095 , 20.000000 , - 4.794176 , - 46.506000 ]
202+ turb_naca0012_sa .test_vals_aarch64 = [- 8.627052 , - 10.377936 , 1.064491 , 0.019710 , 20.000000 , - 1.763093 , 20.000000 , - 4.794073 , - 46.506000 ]
203203 test_list .append (turb_naca0012_sa )
204204
205205 # NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
206206 turb_naca0012_sst = TestCase ('turb_naca0012_sst' )
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 = [- 11.450475 , - 12.797872 , - 5.863655 , 1.049989 , 0.019163 , - 1.856263 ]
211- turb_naca0012_sst .test_vals_aarch64 = [- 11.450473 , - 12.797872 , - 5.863655 , 1.049989 , 0.019163 , - 1.856266 ]
210+ turb_naca0012_sst .test_vals = [- 11.450475 , - 12.797872 , - 5.863655 , 1.049989 , 0.019163 , - 1.856263 , - 38.694000 ]
211+ turb_naca0012_sst .test_vals_aarch64 = [- 11.450473 , - 12.797872 , - 5.863655 , 1.049989 , 0.019163 , - 1.856266 , - 38.694000 ]
212212 test_list .append (turb_naca0012_sst )
213213
214214 # NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
@@ -392,8 +392,8 @@ def main():
392392 inc_poly_cylinder .cfg_dir = "incomp_navierstokes/cylinder"
393393 inc_poly_cylinder .cfg_file = "poly_cylinder.cfg"
394394 inc_poly_cylinder .test_iter = 20
395- inc_poly_cylinder .test_vals = [- 7.851512 , - 2.093420 , 0.029974 , 1.921595 , 0.0 ]
396- inc_poly_cylinder .test_vals_aarch64 = [- 7.851510 , - 2.093419 , 0.029974 , 1.921595 , 0.0 ]
395+ inc_poly_cylinder .test_vals = [- 7.851512 , - 2.093420 , 0.029974 , 1.921595 , - 175.300000 ]
396+ inc_poly_cylinder .test_vals_aarch64 = [- 7.851510 , - 2.093419 , 0.029974 , 1.921595 , - 175.300000 ]
397397 inc_poly_cylinder .new_output = True
398398 test_list .append (inc_poly_cylinder )
399399
@@ -424,7 +424,7 @@ def main():
424424 inc_turb_naca0012_sst_sust .cfg_dir = "incomp_rans/naca0012"
425425 inc_turb_naca0012_sst_sust .cfg_file = "naca0012_SST_SUST.cfg"
426426 inc_turb_naca0012_sst_sust .test_iter = 20
427- inc_turb_naca0012_sst_sust .test_vals = [- 7.276424 , 0.145860 , 0.000003 , 0.312011 , 0.0 ]
427+ inc_turb_naca0012_sst_sust .test_vals = [- 7.276424 , 0.145860 , 0.000003 , 0.312011 ]
428428 test_list .append (inc_turb_naca0012_sst_sust )
429429
430430 ######################################
@@ -457,7 +457,7 @@ def main():
457457 square_cylinder .cfg_dir = "unsteady/square_cylinder"
458458 square_cylinder .cfg_file = "turb_square.cfg"
459459 square_cylinder .test_iter = 3
460- square_cylinder .test_vals = [- 1.162564 , 0.066401 , 1.399788 , 2.220402 , 1.399743 , 2.218603 ]
460+ square_cylinder .test_vals = [- 2.926874 , - 1.406730 , 0.036318 , 1.399116 , 2.199755 , 1.399116 , 2.199755 , - 3.9975e-01 ]
461461 square_cylinder .unsteady = True
462462 test_list .append (square_cylinder )
463463
@@ -486,7 +486,7 @@ def main():
486486 ddes_flatplate .cfg_dir = "ddes/flatplate"
487487 ddes_flatplate .cfg_file = "ddes_flatplate.cfg"
488488 ddes_flatplate .test_iter = 10
489- ddes_flatplate .test_vals = [- 2.714758 , - 5.883004 , - 0.215005 , 0.023783 , 0.0 ]
489+ ddes_flatplate .test_vals = [- 3.826301 , - 6.378282 , - 0.013762 , 0.106606 , - 11664.000000 ]
490490 ddes_flatplate .unsteady = True
491491 test_list .append (ddes_flatplate )
492492
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