@@ -79,7 +79,7 @@ def main():
7979 fixedCL_naca0012 .cfg_dir = "fixed_cl/naca0012"
8080 fixedCL_naca0012 .cfg_file = "inv_NACA0012.cfg"
8181 fixedCL_naca0012 .test_iter = 10
82- fixedCL_naca0012 .test_vals = [- 12.130263 , - 6.703735 , 0.300000 , 0.019470 ]
82+ fixedCL_naca0012 .test_vals = [- 12.130189 , - 6.702728 , 0.300000 , 0.019470 ]
8383 test_list .append (fixedCL_naca0012 )
8484
8585 # HYPERSONIC FLOW PAST BLUNT BODY
@@ -107,31 +107,31 @@ def main():
107107 cylinder .cfg_dir = "navierstokes/cylinder"
108108 cylinder .cfg_file = "lam_cylinder.cfg"
109109 cylinder .test_iter = 25
110- cylinder .test_vals = [- 6.765432 , - 1.297428 , 0.019596 , 0.310245 ]
110+ cylinder .test_vals = [- 6.765432 , - 1.297428 , 0.019596 , 0.310240 ]
111111 test_list .append (cylinder )
112112
113113 # Laminar cylinder (low Mach correction)
114114 cylinder_lowmach = TestCase ('cylinder_lowmach' )
115115 cylinder_lowmach .cfg_dir = "navierstokes/cylinder"
116116 cylinder_lowmach .cfg_file = "cylinder_lowmach.cfg"
117117 cylinder_lowmach .test_iter = 25
118- cylinder_lowmach .test_vals = [- 6.850130 , - 1.388096 , - 0.056203 , 108.140820 ]
118+ cylinder_lowmach .test_vals = [- 6.850130 , - 1.388096 , - 0.056203 , 108.140819 ]
119119 test_list .append (cylinder_lowmach )
120120
121121 # 2D Poiseuille flow (body force driven with periodic inlet / outlet)
122122 poiseuille = TestCase ('poiseuille' )
123123 poiseuille .cfg_dir = "navierstokes/poiseuille"
124124 poiseuille .cfg_file = "lam_poiseuille.cfg"
125125 poiseuille .test_iter = 10
126- poiseuille .test_vals = [- 5.048279 , 0.650817 , 0.008715 , 13.677768 ]
126+ poiseuille .test_vals = [- 5.048282 , 0.650814 , 0.008714 , 13.677678 ]
127127 test_list .append (poiseuille )
128128
129129 # 2D Poiseuille flow (inlet profile file)
130130 poiseuille_profile = TestCase ('poiseuille_profile' )
131131 poiseuille_profile .cfg_dir = "navierstokes/poiseuille"
132132 poiseuille_profile .cfg_file = "profile_poiseuille.cfg"
133133 poiseuille_profile .test_iter = 10
134- poiseuille_profile .test_vals = [- 12.494741 , - 7.712718 , - 0.000000 , 2.085796 ]
134+ poiseuille_profile .test_vals = [- 12.494721 , - 7.712408 , - 0.000000 , 2.085796 ]
135135 test_list .append (poiseuille_profile )
136136
137137 ##########################
@@ -175,31 +175,31 @@ def main():
175175 turb_oneram6 .cfg_dir = "rans/oneram6"
176176 turb_oneram6 .cfg_file = "turb_ONERAM6.cfg"
177177 turb_oneram6 .test_iter = 10
178- turb_oneram6 .test_vals = [- 2.372345 , - 6.579369 , 0.229866 , 0.147638 ]
178+ turb_oneram6 .test_vals = [- 2.372346 , - 6.579370 , 0.229866 , 0.147638 ]
179179 test_list .append (turb_oneram6 )
180180
181181 # NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
182182 turb_naca0012_sa = TestCase ('turb_naca0012_sa' )
183183 turb_naca0012_sa .cfg_dir = "rans/naca0012"
184184 turb_naca0012_sa .cfg_file = "turb_NACA0012_sa.cfg"
185185 turb_naca0012_sa .test_iter = 10
186- turb_naca0012_sa .test_vals = [- 12.076423 , - 16.147693 , 1.064326 , 0.019770 ]
186+ turb_naca0012_sa .test_vals = [- 12.076819 , - 16.049252 , 1.064326 , 0.019770 ]
187187 test_list .append (turb_naca0012_sa )
188188
189189 # NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
190190 turb_naca0012_sst = TestCase ('turb_naca0012_sst' )
191191 turb_naca0012_sst .cfg_dir = "rans/naca0012"
192192 turb_naca0012_sst .cfg_file = "turb_NACA0012_sst.cfg"
193193 turb_naca0012_sst .test_iter = 10
194- turb_naca0012_sst .test_vals = [- 15.273727 , - 6.243780 , 1.049988 , 0.019165 ]
194+ turb_naca0012_sst .test_vals = [- 15.273728 , - 6.243783 , 1.049988 , 0.019165 ]
195195 test_list .append (turb_naca0012_sst )
196196
197197 # NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
198198 turb_naca0012_sst_sust = TestCase ('turb_naca0012_sst_sust' )
199199 turb_naca0012_sst_sust .cfg_dir = "rans/naca0012"
200200 turb_naca0012_sst_sust .cfg_file = "turb_NACA0012_sst_sust.cfg"
201201 turb_naca0012_sst_sust .test_iter = 10
202- turb_naca0012_sst_sust .test_vals = [- 14.851214 , - 6.062557 , 1.005233 , 0.019014 ]
202+ turb_naca0012_sst_sust .test_vals = [- 14.851214 , - 6.062566 , 1.005233 , 0.019014 ]
203203 test_list .append (turb_naca0012_sst_sust )
204204
205205 # PROPELLER
@@ -232,39 +232,39 @@ def main():
232232 turb_naca0012_1c .cfg_dir = "rans_uq/naca0012"
233233 turb_naca0012_1c .cfg_file = "turb_NACA0012_uq_1c.cfg"
234234 turb_naca0012_1c .test_iter = 10
235- turb_naca0012_1c .test_vals = [- 4.906594 , 1.338035 , 6.086178 , 2.412995 ]
235+ turb_naca0012_1c .test_vals = [- 4.906563 , 1.338083 , 6.086180 , 2.412997 ]
236236 test_list .append (turb_naca0012_1c )
237237
238238 # NACA0012 2c
239239 turb_naca0012_2c = TestCase ('turb_naca0012_2c' )
240240 turb_naca0012_2c .cfg_dir = "rans_uq/naca0012"
241241 turb_naca0012_2c .cfg_file = "turb_NACA0012_uq_2c.cfg"
242242 turb_naca0012_2c .test_iter = 10
243- turb_naca0012_2c .test_vals = [- 5.230219 , 1.262228 , 6.086155 , 2.412757 ]
243+ turb_naca0012_2c .test_vals = [- 5.230218 , 1.262228 , 6.086157 , 2.412759 ]
244244 test_list .append (turb_naca0012_2c )
245245
246246 # NACA0012 3c
247247 turb_naca0012_3c = TestCase ('turb_naca0012_3c' )
248248 turb_naca0012_3c .cfg_dir = "rans_uq/naca0012"
249249 turb_naca0012_3c .cfg_file = "turb_NACA0012_uq_3c.cfg"
250250 turb_naca0012_3c .test_iter = 10
251- turb_naca0012_3c .test_vals = [- 5.277130 , 1.246265 , 6.086050 , 2.412462 ]
251+ turb_naca0012_3c .test_vals = [- 5.277130 , 1.246265 , 6.086053 , 2.412464 ]
252252 test_list .append (turb_naca0012_3c )
253253
254254 # NACA0012 p1c1
255255 turb_naca0012_p1c1 = TestCase ('turb_naca0012_p1c1' )
256256 turb_naca0012_p1c1 .cfg_dir = "rans_uq/naca0012"
257257 turb_naca0012_p1c1 .cfg_file = "turb_NACA0012_uq_p1c1.cfg"
258258 turb_naca0012_p1c1 .test_iter = 10
259- turb_naca0012_p1c1 .test_vals = [- 5.012853 , 1.310014 , 6.086064 , 2.412930 ]
259+ turb_naca0012_p1c1 .test_vals = [- 5.012946 , 1.309725 , 6.086066 , 2.412931 ]
260260 test_list .append (turb_naca0012_p1c1 )
261261
262262 # NACA0012 p1c2
263263 turb_naca0012_p1c2 = TestCase ('turb_naca0012_p1c2' )
264264 turb_naca0012_p1c2 .cfg_dir = "rans_uq/naca0012"
265265 turb_naca0012_p1c2 .cfg_file = "turb_NACA0012_uq_p1c2.cfg"
266266 turb_naca0012_p1c2 .test_iter = 10
267- turb_naca0012_p1c2 .test_vals = [- 5.264020 , 1.251315 , 6.086450 , 2.413069 ]
267+ turb_naca0012_p1c2 .test_vals = [- 5.264019 , 1.251314 , 6.086451 , 2.413070 ]
268268 test_list .append (turb_naca0012_p1c2 )
269269
270270 ######################################
@@ -298,15 +298,15 @@ def main():
298298 cavity .cfg_dir = "moving_wall/cavity"
299299 cavity .cfg_file = "lam_cavity.cfg"
300300 cavity .test_iter = 25
301- cavity .test_vals = [- 5.627934 , - 0.164469 , 0.051998 , 2.547062 ]
301+ cavity .test_vals = [- 5.627934 , - 0.164469 , 0.051998 , 2.547065 ]
302302 test_list .append (cavity )
303303
304304 # Spinning cylinder
305305 spinning_cylinder = TestCase ('spinning_cylinder' )
306306 spinning_cylinder .cfg_dir = "moving_wall/spinning_cylinder"
307307 spinning_cylinder .cfg_file = "spinning_cylinder.cfg"
308308 spinning_cylinder .test_iter = 25
309- spinning_cylinder .test_vals = [- 7.996310 , - 2.601760 , 1.510694 , 1.493879 ]
309+ spinning_cylinder .test_vals = [- 7.996313 , - 2.601764 , 1.510692 , 1.493876 ]
310310 test_list .append (spinning_cylinder )
311311
312312 ######################################
@@ -318,7 +318,7 @@ def main():
318318 square_cylinder .cfg_dir = "unsteady/square_cylinder"
319319 square_cylinder .cfg_file = "turb_square.cfg"
320320 square_cylinder .test_iter = 3
321- square_cylinder .test_vals = [- 1.162563 , 0.066395 , 1.399790 , 2.220393 ]
321+ square_cylinder .test_vals = [- 1.162572 , 0.066371 , 1.399790 , 2.220393 ]
322322 square_cylinder .unsteady = True
323323 test_list .append (square_cylinder )
324324
@@ -358,15 +358,15 @@ def main():
358358 edge_VW .cfg_dir = "nicf/edge"
359359 edge_VW .cfg_file = "edge_VW.cfg"
360360 edge_VW .test_iter = 100
361- edge_VW .test_vals = [- 5.040282 , 1.124488 , - 0.000009 , 0.000000 ]
361+ edge_VW .test_vals = [- 5.040283 , 1.124491 , - 0.000009 , 0.000000 ]
362362 test_list .append (edge_VW )
363363
364364 # Rarefaction shock wave edge_PPR
365365 edge_PPR = TestCase ('edge_PPR' )
366366 edge_PPR .cfg_dir = "nicf/edge"
367367 edge_PPR .cfg_file = "edge_PPR.cfg"
368368 edge_PPR .test_iter = 100
369- edge_PPR .test_vals = [- 5.401709 , 0.738096 , - 0.000035 , 0.000000 ]
369+ edge_PPR .test_vals = [- 5.401640 , 0.738165 , - 0.000035 , 0.000000 ]
370370 test_list .append (edge_PPR )
371371
372372 ######################################
@@ -378,7 +378,7 @@ def main():
378378 Jones_tc .cfg_dir = "turbomachinery/APU_turbocharger"
379379 Jones_tc .cfg_file = "Jones.cfg"
380380 Jones_tc .test_iter = 5
381- Jones_tc .test_vals = [- 5.280316 , 0.379652 , 44.725470 , 2.271540 ]
381+ Jones_tc .test_vals = [- 5.280316 , 0.379651 , 44.725470 , 2.271540 ]
382382 Jones_tc .new_output = False
383383 test_list .append (Jones_tc )
384384
@@ -387,7 +387,7 @@ def main():
387387 Jones_tc_rst .cfg_dir = "turbomachinery/APU_turbocharger"
388388 Jones_tc_rst .cfg_file = "Jones_rst.cfg"
389389 Jones_tc_rst .test_iter = 5
390- Jones_tc_rst .test_vals = [- 4.625318 , - 1.569633 , 34.014100 , 10.187650 ]
390+ Jones_tc_rst .test_vals = [- 4.625319 , - 1.569634 , 34.014100 , 10.187660 ]
391391 Jones_tc_rst .new_output = False
392392 test_list .append (Jones_tc_rst )
393393
@@ -396,7 +396,7 @@ def main():
396396 axial_stage2D .cfg_dir = "turbomachinery/axial_stage_2D"
397397 axial_stage2D .cfg_file = "Axial_stage2D.cfg"
398398 axial_stage2D .test_iter = 20
399- axial_stage2D .test_vals = [- 1.933199 , 5.381564 , 73.357910 , 1.780510 ]
399+ axial_stage2D .test_vals = [- 1.933199 , 5.381560 , 73.357900 , 1.780500 ]
400400 axial_stage2D .new_output = False
401401 test_list .append (axial_stage2D )
402402
@@ -405,7 +405,7 @@ def main():
405405 transonic_stator .cfg_dir = "turbomachinery/transonic_stator_2D"
406406 transonic_stator .cfg_file = "transonic_stator.cfg"
407407 transonic_stator .test_iter = 20
408- transonic_stator .test_vals = [- 0.563532 , 5.823231 , 96.736000 , 0.062426 ]
408+ transonic_stator .test_vals = [- 0.563540 , 5.823232 , 96.736080 , 0.062426 ]
409409 transonic_stator .new_output = False
410410 test_list .append (transonic_stator )
411411
@@ -414,7 +414,7 @@ def main():
414414 transonic_stator_rst .cfg_dir = "turbomachinery/transonic_stator_2D"
415415 transonic_stator_rst .cfg_file = "transonic_stator_rst.cfg"
416416 transonic_stator_rst .test_iter = 20
417- transonic_stator_rst .test_vals = [- 6.621624 , - 0.614368 , 5.002986 , 0.002951 ]
417+ transonic_stator_rst .test_vals = [- 6.621626 , - 0.614379 , 5.002986 , 0.002951 ]
418418 transonic_stator_rst .new_output = False
419419 test_list .append (transonic_stator_rst )
420420
@@ -427,7 +427,7 @@ def main():
427427 uniform_flow .cfg_dir = "sliding_interface/uniform_flow"
428428 uniform_flow .cfg_file = "uniform_NN.cfg"
429429 uniform_flow .test_iter = 5
430- uniform_flow .test_vals = [5.000000 , 0.000000 , - 0.188748 , - 10.631524 ]
430+ uniform_flow .test_vals = [5.000000 , 0.000000 , - 0.188748 , - 10.631530 ]
431431 uniform_flow .unsteady = True
432432 uniform_flow .multizone = True
433433 test_list .append (uniform_flow )
@@ -437,7 +437,7 @@ def main():
437437 channel_2D .cfg_dir = "sliding_interface/channel_2D"
438438 channel_2D .cfg_file = "channel_2D_WA.cfg"
439439 channel_2D .test_iter = 2
440- channel_2D .test_vals = [2.000000 , 0.000000 , 0.397938 , 0.352783 , 0.405451 ]
440+ channel_2D .test_vals = [2.000000 , 0.000000 , 0.398089 , 0.352762 , 0.405397 ]
441441 channel_2D .unsteady = True
442442 channel_2D .multizone = True
443443 test_list .append (channel_2D )
@@ -447,7 +447,7 @@ def main():
447447 channel_3D .cfg_dir = "sliding_interface/channel_3D"
448448 channel_3D .cfg_file = "channel_3D_WA.cfg"
449449 channel_3D .test_iter = 2
450- channel_3D .test_vals = [2.000000 , 0.000000 , 0.620157 , 0.505143 , 0.415205 ]
450+ channel_3D .test_vals = [2.000000 , 0.000000 , 0.620151 , 0.505157 , 0.415249 ]
451451 channel_3D .unsteady = True
452452 channel_3D .multizone = True
453453 test_list .append (channel_3D )
@@ -457,7 +457,7 @@ def main():
457457 pipe .cfg_dir = "sliding_interface/pipe"
458458 pipe .cfg_file = "pipe_NN.cfg"
459459 pipe .test_iter = 2
460- pipe .test_vals = [0.150024 , 0.491949 , 0.677756 , 0.963990 , 1.006943 ]
460+ pipe .test_vals = [0.150024 , 0.491949 , 0.677757 , 0.963990 , 1.006944 ]
461461 pipe .unsteady = True
462462 pipe .multizone = True
463463 test_list .append (pipe )
@@ -500,7 +500,7 @@ def main():
500500 statbeam3d .cfg_dir = "fea_fsi/StatBeam_3d"
501501 statbeam3d .cfg_file = "configBeam_3d.cfg"
502502 statbeam3d .test_iter = 0
503- statbeam3d .test_vals = [- 8.500954 , - 8.212289 , - 8.117113 , 64095.000000 ]
503+ statbeam3d .test_vals = [- 2.378370 , - 1.585252 , - 2.028505 , 6.4359e+04 ]
504504 test_list .append (statbeam3d )
505505
506506 # Dynamic beam, 2d
@@ -527,7 +527,7 @@ def main():
527527 stat_fsi .cfg_dir = "fea_fsi/stat_fsi"
528528 stat_fsi .cfg_file = "config.cfg"
529529 stat_fsi .test_iter = 7
530- stat_fsi .test_vals = [- 3.242709 , - 4.866601 , 0.000000 , 11.000000 ]
530+ stat_fsi .test_vals = [- 3.242834 , - 4.866608 , 0.000000 , 11.000000 ]
531531 stat_fsi .multizone = True
532532 test_list .append (stat_fsi )
533533
@@ -536,7 +536,7 @@ def main():
536536 dyn_fsi .cfg_dir = "fea_fsi/dyn_fsi"
537537 dyn_fsi .cfg_file = "config.cfg"
538538 dyn_fsi .test_iter = 4
539- dyn_fsi .test_vals = [- 4.379823 , - 4.005990 , 0.000000 , 0 .000000 ]
539+ dyn_fsi .test_vals = [- 4.379823 , - 4.005990 , 0.000000 , 74 .000000 ]
540540 dyn_fsi .multizone = True
541541 dyn_fsi .unsteady = True
542542 test_list .append (dyn_fsi )
@@ -546,7 +546,7 @@ def main():
546546 stat_fsi_restart .cfg_dir = "fea_fsi/stat_fsi"
547547 stat_fsi_restart .cfg_file = "config_restart.cfg"
548548 stat_fsi_restart .test_iter = 1
549- stat_fsi_restart .test_vals = [- 3.474236 , - 4.250645 , 0.000000 , 35 .000000 ]
549+ stat_fsi_restart .test_vals = [- 3.474239 , - 4.250710 , 0.000000 , 36 .000000 ]
550550 stat_fsi_restart .multizone = True
551551 test_list .append (stat_fsi_restart )
552552
0 commit comments