How to use test_iter method in yandex-tank

Best Python code snippet using yandex-tank

parallel_regression.py

Source:parallel_regression.py Github

copy

Full Screen

1#!/usr/bin/env python2## \file parallel_regression.py3# \brief Python script for automated regression testing of SU2 examples4# \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron5# \version 7.0.6 "Blackbird"6#7# SU2 Project Website: https://su2code.github.io8#9# The SU2 Project is maintained by the SU2 Foundation10# (http://su2foundation.org)11#12# Copyright 2012-2020, SU2 Contributors (cf. AUTHORS.md)13#14# SU2 is free software; you can redistribute it and/or15# modify it under the terms of the GNU Lesser General Public16# License as published by the Free Software Foundation; either17# version 2.1 of the License, or (at your option) any later version.18#19# SU2 is distributed in the hope that it will be useful,20# but WITHOUT ANY WARRANTY; without even the implied warranty of21# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU22# Lesser General Public License for more details.23#24# You should have received a copy of the GNU Lesser General Public25# License along with SU2. If not, see <http://www.gnu.org/licenses/>.26# make print(*args) function available in PY2.6+, does'nt work on PY < 2.627from __future__ import print_function28import sys29from TestCase import TestCase30def main():31 '''This program runs SU2 and ensures that the output matches specified values.32 This will be used to do checks when code is pushed to github33 to make sure nothing is broken. '''34 test_list = []35 ##########################36 ### Compressible Euler ###37 ##########################38 # Channel39 channel = TestCase('channel')40 channel.cfg_dir = "euler/channel"41 channel.cfg_file = "inv_channel_RK.cfg"42 channel.test_iter = 2043 channel.test_vals = [-2.651955, 2.814536, 0.031770, 0.002870] #last 4 columns44 channel.su2_exec = "parallel_computation.py -f"45 channel.timeout = 160046 channel.tol = 0.0000147 test_list.append(channel)48 # NACA001249 naca0012 = TestCase('naca0012')50 naca0012.cfg_dir = "euler/naca0012"51 naca0012.cfg_file = "inv_NACA0012_Roe.cfg"52 naca0012.test_iter = 2053 naca0012.test_vals = [-4.055696, -3.564675, 0.336752, 0.021541] #last 4 columns54 naca0012.su2_exec = "parallel_computation.py -f"55 naca0012.timeout = 160056 naca0012.tol = 0.0000157 test_list.append(naca0012)58 # Supersonic wedge59 wedge = TestCase('wedge')60 wedge.cfg_dir = "euler/wedge"61 wedge.cfg_file = "inv_wedge_HLLC.cfg"62 wedge.test_iter = 2063 wedge.test_vals = [-0.941371, 4.787744, -0.208777, 0.036781] #last 4 columns64 wedge.su2_exec = "parallel_computation.py -f"65 wedge.timeout = 160066 wedge.tol = 0.0000167 test_list.append(wedge)68 # ONERA M6 Wing69 oneram6 = TestCase('oneram6')70 oneram6.cfg_dir = "euler/oneram6"71 oneram6.cfg_file = "inv_ONERAM6.cfg"72 oneram6.test_iter = 1073 oneram6.test_vals = [-10.208444, -9.625586, 0.281704, 0.011821] #last 4 columns74 oneram6.su2_exec = "parallel_computation.py -f"75 oneram6.timeout = 320076 oneram6.tol = 0.0000177 test_list.append(oneram6)78 # Fixed CL NACA001279 fixedCL_naca0012 = TestCase('fixedcl_naca0012')80 fixedCL_naca0012.cfg_dir = "fixed_cl/naca0012"81 fixedCL_naca0012.cfg_file = "inv_NACA0012.cfg"82 fixedCL_naca0012.test_iter = 1083 fixedCL_naca0012.test_vals = [-12.137437, -6.705109, 0.300000, 0.019470] #last 4 columns84 fixedCL_naca0012.su2_exec = "parallel_computation.py -f"85 fixedCL_naca0012.timeout = 160086 fixedCL_naca0012.tol = 0.0000187 test_list.append(fixedCL_naca0012)88 # Polar sweep of the inviscid NACA001289 polar_naca0012 = TestCase('polar_naca0012')90 polar_naca0012.cfg_dir = "polar/naca0012"91 polar_naca0012.cfg_file = "inv_NACA0012.cfg"92 polar_naca0012.polar = True93 polar_naca0012.test_iter = 1094 polar_naca0012.test_vals = [-1.216242, 4.253547, 0.001423, 0.015977] #last 4 columns95 polar_naca0012.su2_exec = "compute_polar.py -i 11"96 polar_naca0012.timeout = 160097 polar_naca0012.tol = 0.0000198 test_list.append(polar_naca0012)99 # HYPERSONIC FLOW PAST BLUNT BODY100 bluntbody = TestCase('bluntbody')101 bluntbody.cfg_dir = "euler/bluntbody"102 bluntbody.cfg_file = "blunt.cfg"103 bluntbody.test_iter = 20104 bluntbody.test_vals = [0.540009, 6.916653, 0.000000, 1.868976] #last 4 columns105 bluntbody.su2_exec = "parallel_computation.py -f"106 bluntbody.timeout = 1600107 bluntbody.tol = 0.00001108 test_list.append(bluntbody)109 ##########################110 ### Compressible N-S ###111 ##########################112 # Laminar flat plate113 flatplate = TestCase('flatplate')114 flatplate.cfg_dir = "navierstokes/flatplate"115 flatplate.cfg_file = "lam_flatplate.cfg"116 flatplate.test_iter = 20117 flatplate.test_vals = [-4.648252, 0.813253, -0.130643, 0.024357] #last 4 columns118 flatplate.su2_exec = "parallel_computation.py -f"119 flatplate.timeout = 1600120 flatplate.tol = 0.00001121 test_list.append(flatplate)122 # Laminar cylinder (steady)123 cylinder = TestCase('cylinder')124 cylinder.cfg_dir = "navierstokes/cylinder"125 cylinder.cfg_file = "lam_cylinder.cfg"126 cylinder.test_iter = 25127 cylinder.test_vals = [-6.759136, -1.291221, 0.107150, 0.853257] #last 4 columns128 cylinder.su2_exec = "parallel_computation.py -f"129 cylinder.timeout = 1600130 cylinder.tol = 0.00001131 test_list.append(cylinder)132 # Laminar cylinder (low Mach correction)133 cylinder_lowmach = TestCase('cylinder_lowmach')134 cylinder_lowmach.cfg_dir = "navierstokes/cylinder"135 cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"136 cylinder_lowmach.test_iter = 25137 cylinder_lowmach.test_vals = [-6.870761, -1.408778, -0.228736, 112.418622] #last 4 columns138 cylinder_lowmach.su2_exec = "parallel_computation.py -f"139 cylinder_lowmach.timeout = 1600140 cylinder_lowmach.tol = 0.00001141 test_list.append(cylinder_lowmach)142 # 2D Poiseuille flow (body force driven with periodic inlet / outlet)143 poiseuille = TestCase('poiseuille')144 poiseuille.cfg_dir = "navierstokes/poiseuille"145 poiseuille.cfg_file = "lam_poiseuille.cfg"146 poiseuille.test_iter = 10147 poiseuille.test_vals = [-5.050864, 0.648220, 0.000349, 13.639525] #last 4 columns148 poiseuille.su2_exec = "parallel_computation.py -f"149 poiseuille.timeout = 1600150 poiseuille.tol = 0.001151 test_list.append(poiseuille)152 # 2D Poiseuille flow (inlet profile file)153 poiseuille_profile = TestCase('poiseuille_profile')154 poiseuille_profile.cfg_dir = "navierstokes/poiseuille"155 poiseuille_profile.cfg_file = "profile_poiseuille.cfg"156 poiseuille_profile.test_iter = 10157 poiseuille_profile.test_vals = [-12.493492, -7.671588, -0.000000, 2.085796] #last 4 columns158 poiseuille_profile.su2_exec = "parallel_computation.py -f"159 poiseuille_profile.timeout = 1600160 poiseuille_profile.tol = 0.00001161 test_list.append(poiseuille_profile)162 ##########################163 ### Compressible RANS ###164 ##########################165 # RAE2822 SA166 rae2822_sa = TestCase('rae2822_sa')167 rae2822_sa.cfg_dir = "rans/rae2822"168 rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"169 rae2822_sa.test_iter = 20170 rae2822_sa.test_vals = [-2.013881, -5.271311, 0.814981, 0.061858] #last 4 columns171 rae2822_sa.su2_exec = "parallel_computation.py -f"172 rae2822_sa.timeout = 1600173 rae2822_sa.tol = 0.00001174 test_list.append(rae2822_sa)175 # RAE2822 SST176 rae2822_sst = TestCase('rae2822_sst')177 rae2822_sst.cfg_dir = "rans/rae2822"178 rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"179 rae2822_sst.test_iter = 20180 rae2822_sst.test_vals = [-0.510623, 4.877370, 0.817050, 0.062058] #last 4 columns181 rae2822_sst.su2_exec = "parallel_computation.py -f"182 rae2822_sst.timeout = 1600183 rae2822_sst.tol = 0.00001184 test_list.append(rae2822_sst)185 # RAE2822 SST_SUST186 rae2822_sst_sust = TestCase('rae2822_sst_sust')187 rae2822_sst_sust.cfg_dir = "rans/rae2822"188 rae2822_sst_sust.cfg_file = "turb_SST_SUST_RAE2822.cfg"189 rae2822_sst_sust.test_iter = 20190 rae2822_sst_sust.test_vals = [-2.430819, 4.877370, 0.817050, 0.062058] #last 4 columns191 rae2822_sst_sust.su2_exec = "parallel_computation.py -f"192 rae2822_sst_sust.timeout = 1600193 rae2822_sst_sust.tol = 0.00001194 test_list.append(rae2822_sst_sust)195 # Flat plate196 turb_flatplate = TestCase('turb_flatplate')197 turb_flatplate.cfg_dir = "rans/flatplate"198 turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"199 turb_flatplate.test_iter = 20200 turb_flatplate.test_vals = [-4.145487, -6.734014, -0.176490, 0.057451] #last 4 columns201 turb_flatplate.su2_exec = "parallel_computation.py -f"202 turb_flatplate.timeout = 1600203 turb_flatplate.tol = 0.00001204 test_list.append(turb_flatplate)205 # ONERA M6 Wing206 turb_oneram6 = TestCase('turb_oneram6')207 turb_oneram6.cfg_dir = "rans/oneram6"208 turb_oneram6.cfg_file = "turb_ONERAM6.cfg"209 turb_oneram6.test_iter = 10210 turb_oneram6.test_vals = [-2.412448, -6.702975, 0.229867, 0.147637] #last 4 columns211 turb_oneram6.su2_exec = "parallel_computation.py -f"212 turb_oneram6.timeout = 3200213 turb_oneram6.tol = 0.00001214 test_list.append(turb_oneram6)215 # NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)216 turb_naca0012_sa = TestCase('turb_naca0012_sa')217 turb_naca0012_sa.cfg_dir = "rans/naca0012"218 turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"219 turb_naca0012_sa.test_iter = 10220 turb_naca0012_sa.test_vals = [-12.078401, -16.147829, 1.064326, 0.019770] #last 4 columns221 turb_naca0012_sa.su2_exec = "parallel_computation.py -f"222 turb_naca0012_sa.timeout = 3200223 turb_naca0012_sa.tol = 0.00001224 test_list.append(turb_naca0012_sa)225 # NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)226 turb_naca0012_sst = TestCase('turb_naca0012_sst')227 turb_naca0012_sst.cfg_dir = "rans/naca0012"228 turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"229 turb_naca0012_sst.test_iter = 10230 turb_naca0012_sst.test_vals = [-15.273461, -6.243802, 1.049988, 0.019165] #last 4 columns231 turb_naca0012_sst.su2_exec = "parallel_computation.py -f"232 turb_naca0012_sst.timeout = 3200233 turb_naca0012_sst.tol = 0.00001234 test_list.append(turb_naca0012_sst)235 # NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)236 turb_naca0012_sst_sust = TestCase('turb_naca0012_sst_sust')237 turb_naca0012_sst_sust.cfg_dir = "rans/naca0012"238 turb_naca0012_sst_sust.cfg_file = "turb_NACA0012_sst_sust.cfg"239 turb_naca0012_sst_sust.test_iter = 10240 turb_naca0012_sst_sust.test_vals = [-14.851212, -6.062226, 1.005233, 0.019014] #last 4 columns241 turb_naca0012_sst_sust.su2_exec = "parallel_computation.py -f"242 turb_naca0012_sst_sust.timeout = 3200243 turb_naca0012_sst_sust.tol = 0.00001244 test_list.append(turb_naca0012_sst_sust)245 # PROPELLER246 propeller = TestCase('propeller')247 propeller.cfg_dir = "rans/propeller"248 propeller.cfg_file = "propeller.cfg"249 propeller.test_iter = 10250 propeller.test_vals = [-3.389575, -8.409529, 0.000048, 0.056329] #last 4 columns251 propeller.su2_exec = "parallel_computation.py -f"252 propeller.timeout = 3200253 propeller.tol = 0.00001254 test_list.append(propeller)255 #################################256 ## Compressible RANS Restart ###257 #################################258 # NACA0012 SST Multigrid restart259 turb_naca0012_sst_restart_mg = TestCase('turb_naca0012_sst_restart_mg')260 turb_naca0012_sst_restart_mg.cfg_dir = "rans/naca0012"261 turb_naca0012_sst_restart_mg.cfg_file = "turb_NACA0012_sst_multigrid_restart.cfg"262 turb_naca0012_sst_restart_mg.test_iter = 20263 turb_naca0012_sst_restart_mg.ntest_vals = 5264 turb_naca0012_sst_restart_mg.test_vals = [-7.627853, -7.729525, -1.981053, -0.000016, 0.079062] #last 5 columns265 turb_naca0012_sst_restart_mg.su2_exec = "parallel_computation.py -f"266 turb_naca0012_sst_restart_mg.timeout = 3200267 turb_naca0012_sst_restart_mg.tol = 0.000001268 test_list.append(turb_naca0012_sst_restart_mg)269 #############################270 ### Incompressible Euler ###271 #############################272 # NACA0012 Hydrofoil273 inc_euler_naca0012 = TestCase('inc_euler_naca0012')274 inc_euler_naca0012.cfg_dir = "incomp_euler/naca0012"275 inc_euler_naca0012.cfg_file = "incomp_NACA0012.cfg"276 inc_euler_naca0012.test_iter = 20277 inc_euler_naca0012.test_vals = [-4.802192, -3.799720, 0.497093, 0.007515] #last 4 columns278 inc_euler_naca0012.su2_exec = "parallel_computation.py -f"279 inc_euler_naca0012.timeout = 1600280 inc_euler_naca0012.tol = 0.00001281 test_list.append(inc_euler_naca0012)282 # C-D nozzle with pressure inlet and mass flow outlet283 inc_nozzle = TestCase('inc_nozzle')284 inc_nozzle.cfg_dir = "incomp_euler/nozzle"285 inc_nozzle.cfg_file = "inv_nozzle.cfg"286 inc_nozzle.test_iter = 20287 inc_nozzle.test_vals = [-5.959953, -4.932037, -0.000109, 0.121192] #last 4 columns288 inc_nozzle.su2_exec = "parallel_computation.py -f"289 inc_nozzle.timeout = 1600290 inc_nozzle.tol = 0.00001291 test_list.append(inc_nozzle)292 #############################293 ### Incompressible N-S ###294 #############################295 # Laminar cylinder296 inc_lam_cylinder = TestCase('inc_lam_cylinder')297 inc_lam_cylinder.cfg_dir = "incomp_navierstokes/cylinder"298 inc_lam_cylinder.cfg_file = "incomp_cylinder.cfg"299 inc_lam_cylinder.test_iter = 10300 inc_lam_cylinder.test_vals = [-3.987107, -3.176477, -0.057813, 7.691336] #last 4 columns301 inc_lam_cylinder.su2_exec = "parallel_computation.py -f"302 inc_lam_cylinder.timeout = 1600303 inc_lam_cylinder.tol = 0.00001304 test_list.append(inc_lam_cylinder)305 # Buoyancy-driven cavity306 inc_buoyancy = TestCase('inc_buoyancy')307 inc_buoyancy.cfg_dir = "incomp_navierstokes/buoyancy_cavity"308 inc_buoyancy.cfg_file = "lam_buoyancy_cavity.cfg"309 inc_buoyancy.test_iter = 20310 inc_buoyancy.test_vals = [-4.436564, 0.508012, 0.000000, 0.000000] #last 4 columns311 inc_buoyancy.su2_exec = "parallel_computation.py -f"312 inc_buoyancy.timeout = 1600313 inc_buoyancy.tol = 0.00001314 test_list.append(inc_buoyancy)315 # Laminar heated cylinder with polynomial fluid model316 inc_poly_cylinder = TestCase('inc_poly_cylinder')317 inc_poly_cylinder.cfg_dir = "incomp_navierstokes/cylinder"318 inc_poly_cylinder.cfg_file = "poly_cylinder.cfg"319 inc_poly_cylinder.test_iter = 20320 inc_poly_cylinder.test_vals = [-7.812686, -2.080649, 0.016033, 1.912088] #last 4 columns321 inc_poly_cylinder.su2_exec = "parallel_computation.py -f"322 inc_poly_cylinder.timeout = 1600323 inc_poly_cylinder.tol = 0.00001324 test_list.append(inc_poly_cylinder)325 # X-coarse laminar bend as a mixed element CGNS test326 inc_lam_bend = TestCase('inc_lam_bend')327 inc_lam_bend.cfg_dir = "incomp_navierstokes/bend"328 inc_lam_bend.cfg_file = "lam_bend.cfg"329 inc_lam_bend.test_iter = 10330 inc_lam_bend.test_vals = [-3.437567, -3.088005, -0.022291, -0.172738] #last 4 columns331 inc_lam_bend.su2_exec = "mpirun -n 2 SU2_CFD"332 inc_lam_bend.timeout = 1600333 inc_lam_bend.tol = 0.00001334 test_list.append(inc_lam_bend)335 ############################336 ### Incompressible RANS ###337 ############################338 # NACA0012339 inc_turb_naca0012 = TestCase('inc_turb_naca0012')340 inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"341 inc_turb_naca0012.cfg_file = "naca0012.cfg"342 inc_turb_naca0012.test_iter = 20343 inc_turb_naca0012.test_vals = [-4.788584, -11.040550, -0.000000, 0.309515] #last 4 columns344 inc_turb_naca0012.su2_exec = "parallel_computation.py -f"345 inc_turb_naca0012.timeout = 1600346 inc_turb_naca0012.tol = 0.00001347 test_list.append(inc_turb_naca0012)348 # NACA0012, SST_SUST349 inc_turb_naca0012_sst_sust = TestCase('inc_turb_naca0012_sst_sust')350 inc_turb_naca0012_sst_sust.cfg_dir = "incomp_rans/naca0012"351 inc_turb_naca0012_sst_sust.cfg_file = "naca0012_SST_SUST.cfg"352 inc_turb_naca0012_sst_sust.test_iter = 20353 inc_turb_naca0012_sst_sust.test_vals = [-7.276480, 0.146181, -0.000000, 0.312017] #last 4 columns354 inc_turb_naca0012_sst_sust.su2_exec = "parallel_computation.py -f"355 inc_turb_naca0012_sst_sust.timeout = 1600356 inc_turb_naca0012_sst_sust.tol = 0.00001357 test_list.append(inc_turb_naca0012_sst_sust)358 ####################359 ### DG-FEM Euler ###360 ####################361 # NACA0012362 fem_euler_naca0012 = TestCase('fem_euler_naca0012')363 fem_euler_naca0012.cfg_dir = "hom_euler/NACA0012_5thOrder"364 fem_euler_naca0012.cfg_file = "fem_NACA0012_reg.cfg"365 fem_euler_naca0012.test_iter = 10366 fem_euler_naca0012.test_vals = [-6.519946,-5.976944,0.255551,0.000028] #last 4 columns367 fem_euler_naca0012.su2_exec = "mpirun -n 2 SU2_CFD"368 fem_euler_naca0012.timeout = 1600369 fem_euler_naca0012.tol = 0.00001370 test_list.append(fem_euler_naca0012)371 ############################372 ### DG-FEM Navier-Stokes ###373 ############################374 # Flat plate375 fem_ns_flatplate = TestCase('fem_ns_flatplate')376 fem_ns_flatplate.cfg_dir = "hom_navierstokes/FlatPlate/nPoly4"377 fem_ns_flatplate.cfg_file = "lam_flatplate_reg.cfg"378 fem_ns_flatplate.test_iter = 25379 fem_ns_flatplate.test_vals = [1.383727,3.175247,0.058387,0.257951] #last 4 columns380 fem_ns_flatplate.su2_exec = "mpirun -n 2 SU2_CFD"381 fem_ns_flatplate.timeout = 1600382 fem_ns_flatplate.tol = 0.00001383 test_list.append(fem_ns_flatplate)384 # Steady cylinder385 fem_ns_cylinder = TestCase('fem_ns_cylinder')386 fem_ns_cylinder.cfg_dir = "hom_navierstokes/CylinderViscous/nPoly3"387 fem_ns_cylinder.cfg_file = "fem_Cylinder_reg.cfg"388 fem_ns_cylinder.test_iter = 10389 fem_ns_cylinder.test_vals = [0.454960,0.979123,-0.000028,79.984799] #last 4 columns390 fem_ns_cylinder.su2_exec = "mpirun -n 2 SU2_CFD"391 fem_ns_cylinder.timeout = 1600392 fem_ns_cylinder.tol = 0.00001393 test_list.append(fem_ns_cylinder)394 # Steady sphere395 fem_ns_sphere = TestCase('fem_ns_sphere')396 fem_ns_sphere.cfg_dir = "hom_navierstokes/SphereViscous/nPoly3_QuadDominant"397 fem_ns_sphere.cfg_file = "fem_Sphere_reg.cfg"398 fem_ns_sphere.test_iter = 10399 fem_ns_sphere.test_vals = [-0.288121,0.240324,0.000258,21.797363] #last 4 columns400 fem_ns_sphere.su2_exec = "SU2_CFD"401 fem_ns_sphere.timeout = 1600402 fem_ns_sphere.tol = 0.00001403 test_list.append(fem_ns_sphere)404 # Unsteady sphere ADER405 fem_ns_sphere_ader = TestCase('fem_ns_sphere_ader')406 fem_ns_sphere_ader.cfg_dir = "hom_navierstokes/SphereViscous/nPoly3_QuadDominant"407 fem_ns_sphere_ader.cfg_file = "fem_Sphere_reg_ADER.cfg"408 fem_ns_sphere_ader.test_iter = 10409 fem_ns_sphere_ader.test_vals = [-35.000000,-35.000000,0.000047,31.110911] #last 4 columns410 fem_ns_sphere_ader.su2_exec = "SU2_CFD"411 fem_ns_sphere_ader.timeout = 1600412 fem_ns_sphere_ader.tol = 0.00001413 test_list.append(fem_ns_sphere_ader)414 # Unsteady cylinder415 fem_ns_unsteady_cylinder = TestCase('fem_ns_unsteady_cylinder')416 fem_ns_unsteady_cylinder.cfg_dir = "hom_navierstokes/UnsteadyCylinder/nPoly4"417 fem_ns_unsteady_cylinder.cfg_file = "fem_unst_cylinder.cfg"418 fem_ns_unsteady_cylinder.test_iter = 11419 fem_ns_unsteady_cylinder.test_vals = [-3.558582,-3.014464,-0.038927,1.383983] #last 4 columns420 fem_ns_unsteady_cylinder.su2_exec = "SU2_CFD"421 fem_ns_unsteady_cylinder.timeout = 1600422 fem_ns_unsteady_cylinder.unsteady = True423 fem_ns_unsteady_cylinder.tol = 0.00001424 test_list.append(fem_ns_unsteady_cylinder)425 # Unsteady cylinder ADER426 fem_ns_unsteady_cylinder_ader = TestCase('fem_ns_unsteady_cylinder_ader')427 fem_ns_unsteady_cylinder_ader.cfg_dir = "hom_navierstokes/UnsteadyCylinder/nPoly4"428 fem_ns_unsteady_cylinder_ader.cfg_file = "fem_unst_cylinder_ADER.cfg"429 fem_ns_unsteady_cylinder_ader.test_iter = 11430 fem_ns_unsteady_cylinder_ader.test_vals = [-35.000000,-35.000000,-0.041003,1.391339] #last 4 columns431 fem_ns_unsteady_cylinder_ader.su2_exec = "SU2_CFD"432 fem_ns_unsteady_cylinder_ader.timeout = 1600433 fem_ns_unsteady_cylinder_ader.unsteady = True434 fem_ns_unsteady_cylinder_ader.tol = 0.00001435 test_list.append(fem_ns_unsteady_cylinder_ader)436 ############################437 ### Transition ###438 ############################439 # Schubauer-Klebanoff Natural Transition Case440 schubauer_klebanoff_transition = TestCase('Schubauer_Klebanoff')441 schubauer_klebanoff_transition.cfg_dir = "transition/Schubauer_Klebanoff"442 schubauer_klebanoff_transition.cfg_file = "transitional_BC_model_ConfigFile.cfg"443 schubauer_klebanoff_transition.test_iter = 10444 schubauer_klebanoff_transition.test_vals = [-7.994738, -14.268367, 0.000046, 0.007987] #last 4 columns445 schubauer_klebanoff_transition.su2_exec = "parallel_computation.py -f"446 schubauer_klebanoff_transition.timeout = 1600447 schubauer_klebanoff_transition.tol = 0.00001448 test_list.append(schubauer_klebanoff_transition)449 #####################################450 ### Cont. adj. compressible Euler ###451 #####################################452 # Inviscid NACA0012453 contadj_naca0012 = TestCase('contadj_naca0012')454 contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"455 contadj_naca0012.cfg_file = "inv_NACA0012.cfg"456 contadj_naca0012.test_iter = 5457 contadj_naca0012.test_vals = [-9.300829, -14.583240, 0.300920, 0.019552] #last 4 columns458 contadj_naca0012.su2_exec = "parallel_computation.py -f"459 contadj_naca0012.timeout = 1600460 contadj_naca0012.tol = 0.00001461 test_list.append(contadj_naca0012)462 # Inviscid ONERA M6463 contadj_oneram6 = TestCase('contadj_oneram6')464 contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"465 contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"466 contadj_oneram6.test_iter = 10467 contadj_oneram6.test_vals = [-12.132202, -12.702416, 0.685900, 0.007594] #last 4 columns468 contadj_oneram6.su2_exec = "parallel_computation.py -f"469 contadj_oneram6.timeout = 1600470 contadj_oneram6.tol = 0.00001471 test_list.append(contadj_oneram6)472 # Inviscid WEDGE: tests averaged outflow total pressure adjoint473 contadj_wedge = TestCase('contadj_wedge')474 contadj_wedge.cfg_dir = "cont_adj_euler/wedge"475 contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"476 contadj_wedge.test_iter = 10477 contadj_wedge.test_vals = [2.872691, -2.755572, 853010.000000, 0.000000] #last 4 columns478 contadj_wedge.su2_exec = "parallel_computation.py -f"479 contadj_wedge.timeout = 1600480 contadj_wedge.tol = 0.00001481 test_list.append(contadj_wedge)482 # Inviscid fixed CL NACA0012483 contadj_fixed_CL_naca0012 = TestCase('contadj_fixedcl_naca0012')484 contadj_fixed_CL_naca0012.cfg_dir = "fixed_cl/naca0012"485 contadj_fixed_CL_naca0012.cfg_file = "inv_NACA0012_ContAdj.cfg"486 contadj_fixed_CL_naca0012.test_iter = 100487 contadj_fixed_CL_naca0012.test_vals = [0.317289, -5.193066, 0.360470, 0.000069] #last 4 columns488 contadj_fixed_CL_naca0012.su2_exec = "parallel_computation.py -f"489 contadj_fixed_CL_naca0012.timeout = 1600490 contadj_fixed_CL_naca0012.tol = 0.00001491 test_list.append(contadj_fixed_CL_naca0012)492 ###################################493 ### Cont. adj. compressible N-S ###494 ###################################495 # Adjoint laminar cylinder496 contadj_ns_cylinder = TestCase('contadj_ns_cylinder')497 contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"498 contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"499 contadj_ns_cylinder.test_iter = 20500 contadj_ns_cylinder.test_vals = [-3.644966, -9.102024, 2.056700, -0.000000] #last 4 columns501 contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"502 contadj_ns_cylinder.timeout = 1600503 contadj_ns_cylinder.tol = 0.00001504 test_list.append(contadj_ns_cylinder)505 # Adjoint laminar naca0012 subsonic506 contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')507 contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"508 contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"509 contadj_ns_naca0012_sub.test_iter = 20510 contadj_ns_naca0012_sub.test_vals = [-2.743268, -8.215193, 0.518810, 0.001210] #last 4 columns511 contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"512 contadj_ns_naca0012_sub.timeout = 1600513 contadj_ns_naca0012_sub.tol = 0.00001514 test_list.append(contadj_ns_naca0012_sub)515 # Adjoint laminar naca0012 transonic516 contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')517 contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"518 contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"519 contadj_ns_naca0012_trans.test_iter = 20520 contadj_ns_naca0012_trans.test_vals = [ -1.039664, -6.575019, 1.772300, 0.012495] #last 4 columns521 contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"522 contadj_ns_naca0012_trans.timeout = 1600523 contadj_ns_naca0012_trans.tol = 0.00001524 test_list.append(contadj_ns_naca0012_trans)525 #######################################################526 ### Cont. adj. compressible RANS (frozen viscosity) ###527 #######################################################528 # Adjoint turbulent NACA0012529 contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')530 contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"531 contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"532 contadj_rans_naca0012.test_iter = 20533 contadj_rans_naca0012.test_vals = [-0.794162, -5.761722, 19.214000, -0.000000] #last 4 columns534 contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"535 contadj_rans_naca0012.timeout = 1600536 contadj_rans_naca0012.tol = 0.00001537 test_list.append(contadj_rans_naca0012)538 # Adjoint turbulent NACA0012 with binary restarts539 contadj_rans_naca0012_bin = TestCase('contadj_rans_naca0012_bin')540 contadj_rans_naca0012_bin.cfg_dir = "cont_adj_rans/naca0012"541 contadj_rans_naca0012_bin.cfg_file = "turb_nasa_binary.cfg"542 contadj_rans_naca0012_bin.test_iter = 18543 contadj_rans_naca0012_bin.test_vals = [-0.794169, -5.761671, 19.214000, -0.000000] #last 4 columns544 contadj_rans_naca0012_bin.su2_exec = "parallel_computation.py -f"545 contadj_rans_naca0012_bin.timeout = 1600546 contadj_rans_naca0012_bin.tol = 0.00001547 test_list.append(contadj_rans_naca0012_bin)548 # Adjoint turbulent RAE2822549 contadj_rans_rae2822 = TestCase('contadj_rans_rae822')550 contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"551 contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"552 contadj_rans_rae2822.test_iter = 20553 contadj_rans_rae2822.test_vals = [-5.381383, -10.883812, -0.212470, 0.005448] #last 4 columns554 contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"555 contadj_rans_rae2822.timeout = 1600556 contadj_rans_rae2822.tol = 0.00001557 test_list.append(contadj_rans_rae2822)558 #############################559 ### Compressibele RANS UQ ###560 #############################561 # NACA0012 1c562 turb_naca0012_1c = TestCase('turb_naca0012_1c')563 turb_naca0012_1c.cfg_dir = "rans_uq/naca0012"564 turb_naca0012_1c.cfg_file = "turb_NACA0012_uq_1c.cfg"565 turb_naca0012_1c.test_iter = 10566 turb_naca0012_1c.test_vals = [-4.973604, 1.141377, 0.870252, 0.041511] #last 4 columns567 turb_naca0012_1c.su2_exec = "parallel_computation.py -f"568 turb_naca0012_1c.timeout = 1600569 turb_naca0012_1c.tol = 0.00001570 test_list.append(turb_naca0012_1c)571 # NACA0012 2c572 turb_naca0012_2c = TestCase('turb_naca0012_2c')573 turb_naca0012_2c.cfg_dir = "rans_uq/naca0012"574 turb_naca0012_2c.cfg_file = "turb_NACA0012_uq_2c.cfg"575 turb_naca0012_2c.test_iter = 10576 turb_naca0012_2c.test_vals = [-5.484222, 0.967203, 0.909852, 0.056844] #last 4 columns577 turb_naca0012_2c.su2_exec = "parallel_computation.py -f"578 turb_naca0012_2c.timeout = 1600579 turb_naca0012_2c.tol = 0.00001580 test_list.append(turb_naca0012_2c)581 # NACA0012 3c582 turb_naca0012_3c = TestCase('turb_naca0012_3c')583 turb_naca0012_3c.cfg_dir = "rans_uq/naca0012"584 turb_naca0012_3c.cfg_file = "turb_NACA0012_uq_3c.cfg"585 turb_naca0012_3c.test_iter = 10586 turb_naca0012_3c.test_vals = [-5.587082, 0.929251, 1.008548, 0.094463] #last 4 columns587 turb_naca0012_3c.su2_exec = "parallel_computation.py -f"588 turb_naca0012_3c.timeout = 1600589 turb_naca0012_3c.tol = 0.00001590 test_list.append(turb_naca0012_3c)591 # NACA0012 p1c1592 turb_naca0012_p1c1 = TestCase('turb_naca0012_p1c1')593 turb_naca0012_p1c1.cfg_dir = "rans_uq/naca0012"594 turb_naca0012_p1c1.cfg_file = "turb_NACA0012_uq_p1c1.cfg"595 turb_naca0012_p1c1.test_iter = 10596 turb_naca0012_p1c1.test_vals = [-5.128243, 1.076374, 0.959431, 0.067416] #last 4 columns597 turb_naca0012_p1c1.su2_exec = "parallel_computation.py -f"598 turb_naca0012_p1c1.timeout = 1600599 turb_naca0012_p1c1.tol = 0.00001600 test_list.append(turb_naca0012_p1c1)601 # NACA0012 p1c2602 turb_naca0012_p1c2 = TestCase('turb_naca0012_p1c2')603 turb_naca0012_p1c2.cfg_dir = "rans_uq/naca0012"604 turb_naca0012_p1c2.cfg_file = "turb_NACA0012_uq_p1c2.cfg"605 turb_naca0012_p1c2.test_iter = 10606 turb_naca0012_p1c2.test_vals = [-5.556656, 0.941889, 0.956330, 0.069297] #last 4 columns607 turb_naca0012_p1c2.su2_exec = "parallel_computation.py -f"608 turb_naca0012_p1c2.timeout = 1600609 turb_naca0012_p1c2.tol = 0.00001610 test_list.append(turb_naca0012_p1c2)611 ######################################612 ### Harmonic Balance ###613 ######################################614 # Description of the regression test615 harmonic_balance = TestCase('harmonic_balance')616 harmonic_balance.cfg_dir = "harmonic_balance"617 harmonic_balance.cfg_file = "HB.cfg"618 harmonic_balance.test_iter = 25619 harmonic_balance.test_vals = [-1.589755, 3.922208, 0.006724, 0.099454] #last 4 columns620 harmonic_balance.su2_exec = "parallel_computation.py -f"621 harmonic_balance.timeout = 1600622 harmonic_balance.tol = 0.00001623 harmonic_balance.new_output = False624 test_list.append(harmonic_balance)625 # Turbulent pitching NACA 64a010 airfoil626 hb_rans_preconditioning = TestCase('hb_rans_preconditioning')627 hb_rans_preconditioning.cfg_dir = "harmonic_balance/hb_rans_preconditioning"628 hb_rans_preconditioning.cfg_file = "davis.cfg"629 hb_rans_preconditioning.test_iter = 25630 hb_rans_preconditioning.test_vals = [-1.909596, -5.954720, 0.007773, 0.131219] #last 4 columns631 hb_rans_preconditioning.su2_exec = "parallel_computation.py -f"632 hb_rans_preconditioning.timeout = 1600633 hb_rans_preconditioning.tol = 0.00001634 hb_rans_preconditioning.new_output = False635 test_list.append(hb_rans_preconditioning)636 ######################################637 ### Moving Wall ###638 ######################################639 # Rotating NACA 0012640 rot_naca0012 = TestCase('rot_naca0012')641 rot_naca0012.cfg_dir = "rotating/naca0012"642 rot_naca0012.cfg_file = "rot_NACA0012.cfg"643 rot_naca0012.test_iter = 25644 rot_naca0012.test_vals = [-2.676869, 2.865489, -0.079572, 0.002267] #last 4 columns645 rot_naca0012.su2_exec = "parallel_computation.py -f"646 rot_naca0012.timeout = 1600647 rot_naca0012.tol = 0.00001648 test_list.append(rot_naca0012)649 # Lid-driven cavity650 cavity = TestCase('cavity')651 cavity.cfg_dir = "moving_wall/cavity"652 cavity.cfg_file = "lam_cavity.cfg"653 cavity.test_iter = 25654 cavity.test_vals = [-5.588455, -0.124966, 0.308126, 0.940895] #last 4 columns655 cavity.su2_exec = "parallel_computation.py -f"656 cavity.timeout = 1600657 cavity.tol = 0.00001658 test_list.append(cavity)659 # Spinning cylinder660 spinning_cylinder = TestCase('spinning_cylinder')661 spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"662 spinning_cylinder.cfg_file = "spinning_cylinder.cfg"663 spinning_cylinder.test_iter = 25664 spinning_cylinder.test_vals = [-7.857785, -2.425289, 1.554359, 1.531183] #last 4 columns665 spinning_cylinder.su2_exec = "parallel_computation.py -f"666 spinning_cylinder.timeout = 1600667 spinning_cylinder.tol = 0.00001668 test_list.append(spinning_cylinder)669 ######################################670 ### Unsteady ###671 ######################################672 # Square cylinder673 square_cylinder = TestCase('square_cylinder')674 square_cylinder.cfg_dir = "unsteady/square_cylinder"675 square_cylinder.cfg_file = "turb_square.cfg"676 square_cylinder.test_iter = 3677 square_cylinder.test_vals = [-1.162660, 0.066413, 1.399789, 2.220408] #last 4 columns678 square_cylinder.su2_exec = "parallel_computation.py -f"679 square_cylinder.timeout = 1600680 square_cylinder.tol = 0.00001681 square_cylinder.unsteady = True682 test_list.append(square_cylinder)683 # Gust684 sine_gust = TestCase('sine_gust')685 sine_gust.cfg_dir = "gust"686 sine_gust.cfg_file = "inv_gust_NACA0012.cfg"687 sine_gust.test_iter = 5688 sine_gust.test_vals = [-1.977520, 3.481804, -0.012343, -0.007390] #last 4 columns689 sine_gust.su2_exec = "parallel_computation.py -f"690 sine_gust.timeout = 1600691 sine_gust.tol = 0.00001692 sine_gust.unsteady = True693 test_list.append(sine_gust)694 # Aeroelastic695 aeroelastic = TestCase('aeroelastic')696 aeroelastic.cfg_dir = "aeroelastic"697 aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"698 aeroelastic.test_iter = 2699 aeroelastic.test_vals = [0.076842, 0.033154, -0.001650, -0.000127] #last 4 columns700 aeroelastic.su2_exec = "parallel_computation.py -f"701 aeroelastic.timeout = 1600702 aeroelastic.tol = 0.00001703 aeroelastic.unsteady = True704 test_list.append(aeroelastic)705 # Delayed Detached Eddy Simulation706 ddes_flatplate = TestCase('ddes_flatplate')707 ddes_flatplate.cfg_dir = "ddes/flatplate"708 ddes_flatplate.cfg_file = "ddes_flatplate.cfg"709 ddes_flatplate.test_iter = 10710 ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783] #last 4 columns711 ddes_flatplate.su2_exec = "parallel_computation.py -f"712 ddes_flatplate.timeout = 1600713 ddes_flatplate.tol = 0.00001714 ddes_flatplate.unsteady = True715 test_list.append(ddes_flatplate)716 # unsteady pitching NACA0015, SA717 unst_inc_turb_naca0015_sa = TestCase('unst_inc_turb_naca0015_sa')718 unst_inc_turb_naca0015_sa.cfg_dir = "unsteady/pitching_naca0015_rans_inc"719 unst_inc_turb_naca0015_sa.cfg_file = "config_incomp_turb_sa.cfg"720 unst_inc_turb_naca0015_sa.test_iter = 1721 unst_inc_turb_naca0015_sa.test_vals = [-2.990703, -6.865923, 1.475736, 0.419770] #last 4 columns722 unst_inc_turb_naca0015_sa.su2_exec = "parallel_computation.py -f"723 unst_inc_turb_naca0015_sa.timeout = 1600724 unst_inc_turb_naca0015_sa.tol = 0.00001725 unst_inc_turb_naca0015_sa.unsteady = True726 test_list.append(unst_inc_turb_naca0015_sa)727 ######################################728 ### NICFD ###729 ######################################730 # Rarefaction shock wave edge_VW731 edge_VW = TestCase('edge_VW')732 edge_VW.cfg_dir = "nicf/edge"733 edge_VW.cfg_file = "edge_VW.cfg"734 edge_VW.test_iter = 100735 edge_VW.test_vals = [-5.203154, 0.933157, -0.000009, 0.000000] #last 4 columns736 edge_VW.su2_exec = "parallel_computation.py -f"737 edge_VW.timeout = 1600738 edge_VW.tol = 0.00001739 test_list.append(edge_VW)740 # Rarefaction shock wave edge_PPR741 edge_PPR = TestCase('edge_PPR')742 edge_PPR.cfg_dir = "nicf/edge"743 edge_PPR.cfg_file = "edge_PPR.cfg"744 edge_PPR.test_iter = 100745 edge_PPR.test_vals = [-5.385223, 0.755862, -0.000035, 0.000000] #last 4 columns746 edge_PPR.su2_exec = "parallel_computation.py -f"747 edge_PPR.timeout = 1600748 edge_PPR.tol = 0.00001749 test_list.append(edge_PPR)750 ######################################751 ### Turbomachinery ###752 ######################################753 # Jones APU Turbocharger754 Jones_tc = TestCase('jones_turbocharger')755 Jones_tc.cfg_dir = "turbomachinery/APU_turbocharger"756 Jones_tc.cfg_file = "Jones.cfg"757 Jones_tc.test_iter = 5758 Jones_tc.test_vals = [-5.280323, 0.379654, 44.725390, 2.271597] #last 4 columns759 Jones_tc.su2_exec = "parallel_computation.py -f"760 Jones_tc.timeout = 1600761 Jones_tc.new_output = False762 Jones_tc.tol = 0.00001763 test_list.append(Jones_tc)764 # Jones APU Turbocharger restart765 Jones_tc_rst = TestCase('jones_turbocharger_restart')766 Jones_tc_rst.cfg_dir = "turbomachinery/APU_turbocharger"767 Jones_tc_rst.cfg_file = "Jones_rst.cfg"768 Jones_tc_rst.test_iter = 5769 Jones_tc_rst.test_vals = [-4.626538, -1.570728, 34.013520, 10.190740] #last 4 columns770 Jones_tc_rst.su2_exec = "parallel_computation.py -f"771 Jones_tc_rst.timeout = 1600772 Jones_tc_rst.new_output = False773 Jones_tc_rst.tol = 0.00001774 test_list.append(Jones_tc_rst)775 # 2D axial stage776 axial_stage2D = TestCase('axial_stage2D')777 axial_stage2D.cfg_dir = "turbomachinery/axial_stage_2D"778 axial_stage2D.cfg_file = "Axial_stage2D.cfg"779 axial_stage2D.test_iter = 20780 axial_stage2D.test_vals = [-1.933205, 5.381311, 73.357930, 1.780467] #last 4 columns781 axial_stage2D.su2_exec = "parallel_computation.py -f"782 axial_stage2D.timeout = 1600783 axial_stage2D.new_output = False784 axial_stage2D.tol = 0.00001785 test_list.append(axial_stage2D)786 # 2D transonic stator787 transonic_stator = TestCase('transonic_stator')788 transonic_stator.cfg_dir = "turbomachinery/transonic_stator_2D"789 transonic_stator.cfg_file = "transonic_stator.cfg"790 transonic_stator.test_iter = 20791 transonic_stator.test_vals = [-0.576128, 5.820136, 96.994800, 0.062868] #last 4 columns792 transonic_stator.su2_exec = "parallel_computation.py -f"793 transonic_stator.timeout = 1600794 transonic_stator.new_output = False795 transonic_stator.tol = 0.00001796 test_list.append(transonic_stator)797 # 2D transonic stator restart798 transonic_stator_rst = TestCase('transonic_stator_restart')799 transonic_stator_rst.cfg_dir = "turbomachinery/transonic_stator_2D"800 transonic_stator_rst.cfg_file = "transonic_stator_rst.cfg"801 transonic_stator_rst.test_iter = 20802 transonic_stator_rst.test_vals = [-6.618297, -0.617100, 5.002986, 0.002951] #last 4 columns803 transonic_stator_rst.su2_exec = "parallel_computation.py -f"804 transonic_stator_rst.timeout = 1600805 transonic_stator_rst.new_output = False806 transonic_stator_rst.tol = 0.00001807 test_list.append(transonic_stator_rst)808 ######################################809 ### Sliding Mesh ###810 ######################################811 # Uniform flow812 uniform_flow = TestCase('uniform_flow')813 uniform_flow.cfg_dir = "sliding_interface/uniform_flow"814 uniform_flow.cfg_file = "uniform_NN.cfg"815 uniform_flow.test_iter = 5816 uniform_flow.test_vals = [5.000000, 0.000000, -0.188747, -10.631534] #last 4 columns817 uniform_flow.su2_exec = "parallel_computation.py -f"818 uniform_flow.timeout = 1600819 uniform_flow.tol = 0.000001820 uniform_flow.unsteady = True821 uniform_flow.multizone = True822 test_list.append(uniform_flow)823 # Channel_2D824 channel_2D = TestCase('channel_2D')825 channel_2D.cfg_dir = "sliding_interface/channel_2D"826 channel_2D.cfg_file = "channel_2D_WA.cfg"827 channel_2D.test_iter = 2828 channel_2D.test_vals = [2.000000, 0.000000, 0.397891, 0.352785, 0.405448] #last 4 columns829 channel_2D.su2_exec = "parallel_computation.py -f"830 channel_2D.timeout = 100831 channel_2D.tol = 0.00001832 channel_2D.unsteady = True833 channel_2D.multizone = True834 test_list.append(channel_2D)835 # Channel_3D836 channel_3D = TestCase('channel_3D')837 channel_3D.cfg_dir = "sliding_interface/channel_3D"838 channel_3D.cfg_file = "channel_3D_WA.cfg"839 channel_3D.test_iter = 2840 channel_3D.test_vals = [2.000000, 0.000000, 0.620166, 0.505156, 0.415129] #last 4 columns841 channel_3D.su2_exec = "parallel_computation.py -f"842 channel_3D.timeout = 1600843 channel_3D.tol = 0.00001844 channel_3D.unsteady = True845 channel_3D.multizone = True846 test_list.append(channel_3D)847 # Pipe848 pipe = TestCase('pipe')849 pipe.cfg_dir = "sliding_interface/pipe"850 pipe.cfg_file = "pipe_NN.cfg"851 pipe.test_iter = 2852 pipe.test_vals = [0.150025, 0.491954, 0.677756, 0.963980, 1.006936] #last 4 columns853 pipe.su2_exec = "parallel_computation.py -f"854 pipe.timeout = 1600855 pipe.tol = 0.00001856 pipe.unsteady = True857 pipe.multizone = True858 test_list.append(pipe)859 # Rotating cylinders860 rotating_cylinders = TestCase('rotating_cylinders')861 rotating_cylinders.cfg_dir = "sliding_interface/rotating_cylinders"862 rotating_cylinders.cfg_file = "rot_cylinders_WA.cfg"863 rotating_cylinders.test_iter = 3864 rotating_cylinders.test_vals = [3.000000, 0.000000, 0.777575, 1.134804, 1.224136] #last 4 columns865 rotating_cylinders.su2_exec = "parallel_computation.py -f"866 rotating_cylinders.timeout = 1600867 rotating_cylinders.tol = 0.00001868 rotating_cylinders.unsteady = True869 rotating_cylinders.multizone = True870 test_list.append(rotating_cylinders)871 # Supersonic vortex shedding872 supersonic_vortex_shedding = TestCase('supersonic_vortex_shedding')873 supersonic_vortex_shedding.cfg_dir = "sliding_interface/supersonic_vortex_shedding"874 supersonic_vortex_shedding.cfg_file = "sup_vor_shed_WA.cfg"875 supersonic_vortex_shedding.test_iter = 5876 supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.227386, 1.638722] #last 4 columns877 supersonic_vortex_shedding.su2_exec = "parallel_computation.py -f"878 supersonic_vortex_shedding.timeout = 1600879 supersonic_vortex_shedding.tol = 0.00001880 supersonic_vortex_shedding.unsteady = True881 supersonic_vortex_shedding.multizone = True882 test_list.append(supersonic_vortex_shedding)883 # Bars_SST_2D884 bars_SST_2D = TestCase('bars_SST_2D')885 bars_SST_2D.cfg_dir = "sliding_interface/bars_SST_2D"886 bars_SST_2D.cfg_file = "bars.cfg"887 bars_SST_2D.test_iter = 13888 bars_SST_2D.test_vals = [13.000000, -0.619179, -1.564701] #last 4 columns889 bars_SST_2D.su2_exec = "SU2_CFD"890 bars_SST_2D.timeout = 1600891 bars_SST_2D.tol = 0.00001892 bars_SST_2D.multizone = True893 test_list.append(bars_SST_2D)894 # Sliding mesh with incompressible flows (steady)895 slinc_steady = TestCase('slinc_steady')896 slinc_steady.cfg_dir = "sliding_interface/incompressible_steady"897 slinc_steady.cfg_file = "config.cfg"898 slinc_steady.test_iter = 19899 slinc_steady.test_vals = [19.000000, -1.766116, -2.206522] #last 4 columns900 slinc_steady.su2_exec = "SU2_CFD"901 slinc_steady.timeout = 100902 slinc_steady.tol = 0.00002903 slinc_steady.multizone = True904 test_list.append(slinc_steady)905 # Sliding mesh with incompressible flows (unsteady)906 # slinc_unsteady = TestCase('slinc_unsteady')907 # slinc_unsteady.cfg_dir = "sliding_interface/incompressible_unsteady"908 # slinc_unsteady.cfg_file = "config.cfg"909 # slinc_unsteady.test_iter = 19910 # slinc_unsteady.test_vals = [-3.513701,1.931626,0.000000,0.000000] #last 4 columns911 # slinc_unsteady.su2_exec = "SU2_CFD"912 # slinc_unsteady.timeout = 100913 # slinc_unsteady.tol = 0.00001914 # slinc_unsteady.unsteady = True915 # test_list.append(slinc_unsteady)916 ##########################917 ### FEA - FSI ###918 ##########################919 # Static beam, 3d920 statbeam3d = TestCase('statbeam3d')921 statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"922 statbeam3d.cfg_file = "configBeam_3d.cfg"923 statbeam3d.test_iter = 0924 statbeam3d.test_vals = [-8.396797, -8.162206, -8.156102, 64095.0] #last 4 columns925 statbeam3d.su2_exec = "parallel_computation_fsi.py -f"926 statbeam3d.timeout = 1600927 statbeam3d.tol = 0.00001928 test_list.append(statbeam3d)929 # Dynamic beam, 2d930 dynbeam2d = TestCase('dynbeam2d')931 dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"932 dynbeam2d.cfg_file = "configBeam_2d.cfg"933 dynbeam2d.test_iter = 6934 dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 6.6127e+04] #last 4 columns935 dynbeam2d.su2_exec = "parallel_computation.py -f"936 dynbeam2d.timeout = 1600937 dynbeam2d.unsteady = True938 dynbeam2d.tol = 0.00001939 test_list.append(dynbeam2d)940 # FSI, 2d941 fsi2d = TestCase('fsi2d')942 fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"943 fsi2d.cfg_file = "configFSI.cfg"944 fsi2d.test_iter = 4945 fsi2d.test_vals = [4, 0, -3.764076, -4.081142] #last 4 columns946 fsi2d.su2_exec = "parallel_computation_fsi.py -f"947 fsi2d.timeout = 1600948 fsi2d.multizone= True949 fsi2d.unsteady = True950 fsi2d.tol = 0.00001951 test_list.append(fsi2d)952 # FSI, Static, 2D, new mesh solver953 stat_fsi = TestCase('stat_fsi')954 stat_fsi.cfg_dir = "fea_fsi/stat_fsi"955 stat_fsi.cfg_file = "config.cfg"956 stat_fsi.test_iter = 7957 stat_fsi.test_vals = [-3.313612, -4.957573, 0.000000, 7.000000] #last 4 columns958 stat_fsi.su2_exec = "mpirun -n 2 SU2_CFD"959 stat_fsi.multizone = True960 stat_fsi.timeout = 1600961 stat_fsi.tol = 0.00001962 test_list.append(stat_fsi)963 # FSI, Dynamic, 2D, new mesh solver964 dyn_fsi = TestCase('dyn_fsi')965 dyn_fsi.cfg_dir = "fea_fsi/dyn_fsi"966 dyn_fsi.cfg_file = "config.cfg"967 dyn_fsi.test_iter = 4968 dyn_fsi.test_vals = [-4.379832, -4.005999, 0.000000, 0.000000] #last 4 columns969 dyn_fsi.multizone = True970 dyn_fsi.unsteady = True971 dyn_fsi.su2_exec = "mpirun -n 2 SU2_CFD"972 dyn_fsi.timeout = 1600973 dyn_fsi.tol = 0.00001974 test_list.append(dyn_fsi)975 # FSI, Static, 2D, new mesh solver, restart976 stat_fsi_restart = TestCase('stat_fsi_restart')977 stat_fsi_restart.cfg_dir = "fea_fsi/stat_fsi"978 stat_fsi_restart.cfg_file = "config_restart.cfg"979 stat_fsi_restart.test_iter = 1980 stat_fsi_restart.test_vals = [-3.422425, -4.289201, 0.000000, 27.000000] #last 4 columns981 stat_fsi_restart.su2_exec = "mpirun -n 2 SU2_CFD"982 stat_fsi_restart.multizone = True983 stat_fsi_restart.timeout = 1600984 stat_fsi_restart.tol = 0.00001985 test_list.append(stat_fsi_restart)986 # ###############################987 # ### Radiative Heat Transfer ###988 # ###############################989 # Radiative heat transfer990 p1rad = TestCase('p1rad')991 p1rad.cfg_dir = "radiation/p1model"992 p1rad.cfg_file = "configp1.cfg"993 p1rad.new_output= True994 p1rad.test_iter = 100995 p1rad.test_vals = [-7.743540, -7.919958, -2.112177, 0.096091] #last 4 columns996 p1rad.su2_exec = "mpirun -n 2 SU2_CFD"997 p1rad.timeout = 1600998 p1rad.tol = 0.00001999 test_list.append(p1rad)1000 # ###############################1001 # ### Conjugate heat transfer ###1002 # ###############################1003 # CHT incompressible1004 cht_incompressible = TestCase('cht_incompressible')1005 cht_incompressible.cfg_dir = "coupled_cht/incomp_2d"1006 cht_incompressible.cfg_file = "cht_2d_3cylinders.cfg"1007 cht_incompressible.test_iter = 101008 cht_incompressible.test_vals = [-2.132187, -0.579649, -0.579649, -0.579649] #last 4 columns1009 cht_incompressible.su2_exec = "SU2_CFD"1010 cht_incompressible.timeout = 16001011 cht_incompressible.multizone = True1012 cht_incompressible.tol = 0.000011013 test_list.append(cht_incompressible)1014 # CHT incompressible unsteady1015 cht_incompressible_unsteady = TestCase('cht_incompressible_unsteady')1016 cht_incompressible_unsteady.cfg_dir = "coupled_cht/incomp_2d_unsteady"1017 cht_incompressible_unsteady.cfg_file = "cht_2d_3cylinders.cfg"1018 cht_incompressible_unsteady.test_iter = 21019 cht_incompressible_unsteady.test_vals = [-1.356091, -0.080383, -0.080387, -0.080384] #last 4 columns1020 cht_incompressible_unsteady.su2_exec = "SU2_CFD"1021 cht_incompressible_unsteady.timeout = 16001022 cht_incompressible_unsteady.multizone = True1023 cht_incompressible_unsteady.unsteady = True1024 cht_incompressible_unsteady.tol = 0.000011025 test_list.append(cht_incompressible_unsteady)1026 # CHT compressible1027 cht_compressible = TestCase('cht_compressible')1028 cht_compressible.cfg_dir = "coupled_cht/comp_2d"1029 cht_compressible.cfg_file = "cht_2d_3cylinders.cfg"1030 cht_compressible.test_iter = 101031 cht_compressible.test_vals = [-4.257607, -0.526125, -0.526125, -0.526125] #last 4 columns1032 cht_compressible.su2_exec = "SU2_CFD"1033 cht_compressible.timeout = 16001034 cht_compressible.multizone = True1035 cht_compressible.tol = 0.000011036 test_list.append(cht_compressible)1037 ##########################1038 ### Python wrapper ###1039 ##########################1040 # NACA00121041 pywrapper_naca0012 = TestCase('pywrapper_naca0012')1042 pywrapper_naca0012.cfg_dir = "euler/naca0012"1043 pywrapper_naca0012.cfg_file = "inv_NACA0012_Roe.cfg"1044 pywrapper_naca0012.test_iter = 1001045 pywrapper_naca0012.test_vals = [-7.298733, -6.733533, 0.333456, 0.021233] #last 4 columns1046 pywrapper_naca0012.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"1047 pywrapper_naca0012.timeout = 16001048 pywrapper_naca0012.tol = 0.000011049 test_list.append(pywrapper_naca0012)1050 # NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)1051 pywrapper_turb_naca0012_sst = TestCase('pywrapper_turb_naca0012_sst')1052 pywrapper_turb_naca0012_sst.cfg_dir = "rans/naca0012"1053 pywrapper_turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"1054 pywrapper_turb_naca0012_sst.test_iter = 101055 pywrapper_turb_naca0012_sst.test_vals = [-15.273461, -6.243802, 1.049988, 0.019165] #last 4 columns1056 pywrapper_turb_naca0012_sst.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"1057 pywrapper_turb_naca0012_sst.timeout = 32001058 pywrapper_turb_naca0012_sst.tol = 0.000011059 test_list.append(pywrapper_turb_naca0012_sst)1060 # Square cylinder1061 pywrapper_square_cylinder = TestCase('pywrapper_square_cylinder')1062 pywrapper_square_cylinder.cfg_dir = "unsteady/square_cylinder"1063 pywrapper_square_cylinder.cfg_file = "turb_square.cfg"1064 pywrapper_square_cylinder.test_iter = 31065 pywrapper_square_cylinder.test_vals = [-1.162660, 0.066413, 1.399789, 2.220408] #last 4 columns1066 pywrapper_square_cylinder.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"1067 pywrapper_square_cylinder.timeout = 16001068 pywrapper_square_cylinder.tol = 0.000011069 pywrapper_square_cylinder.unsteady = True1070 test_list.append(pywrapper_square_cylinder)1071 # Aeroelastic1072 pywrapper_aeroelastic = TestCase('pywrapper_aeroelastic')1073 pywrapper_aeroelastic.cfg_dir = "aeroelastic"1074 pywrapper_aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"1075 pywrapper_aeroelastic.test_iter = 21076 pywrapper_aeroelastic.test_vals = [0.076842, 0.033154, -0.001650, -0.000127] #last 4 columns1077 pywrapper_aeroelastic.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"1078 pywrapper_aeroelastic.timeout = 16001079 pywrapper_aeroelastic.tol = 0.000011080 pywrapper_aeroelastic.unsteady = True1081 test_list.append(pywrapper_aeroelastic)1082 # FSI, 2d1083 pywrapper_fsi2d = TestCase('pywrapper_fsi2d')1084 pywrapper_fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"1085 pywrapper_fsi2d.cfg_file = "configFSI.cfg"1086 pywrapper_fsi2d.test_iter = 41087 pywrapper_fsi2d.test_vals = [4, 0, -3.764076, -4.081142] #last 4 columns1088 pywrapper_fsi2d.su2_exec = "mpirun -np 2 SU2_CFD.py --nZone 2 --fsi True --parallel -f"1089 pywrapper_fsi2d.timeout = 16001090 pywrapper_fsi2d.unsteady = True1091 pywrapper_fsi2d.multizone = True1092 pywrapper_fsi2d.tol = 0.000011093 test_list.append(pywrapper_fsi2d)1094 # Unsteady CHT1095 pywrapper_unsteadyCHT = TestCase('pywrapper_unsteadyCHT')1096 pywrapper_unsteadyCHT.cfg_dir = "py_wrapper/flatPlate_unsteady_CHT"1097 pywrapper_unsteadyCHT.cfg_file = "unsteady_CHT_FlatPlate_Conf.cfg"1098 pywrapper_unsteadyCHT.test_iter = 51099 pywrapper_unsteadyCHT.test_vals = [-1.614167, 2.245730, -0.000767, 0.175598] #last 4 columns1100 pywrapper_unsteadyCHT.su2_exec = "mpirun -np 2 python launch_unsteady_CHT_FlatPlate.py --parallel -f"1101 pywrapper_unsteadyCHT.timeout = 16001102 pywrapper_unsteadyCHT.tol = 0.000011103 pywrapper_unsteadyCHT.unsteady = True1104 pywrapper_unsteadyCHT.new_output = True1105 test_list.append(pywrapper_unsteadyCHT)1106 # Rigid motion1107 pywrapper_rigidMotion = TestCase('pywrapper_rigidMotion')1108 pywrapper_rigidMotion.cfg_dir = "py_wrapper/flatPlate_rigidMotion"1109 pywrapper_rigidMotion.cfg_file = "flatPlate_rigidMotion_Conf.cfg"1110 pywrapper_rigidMotion.test_iter = 51111 pywrapper_rigidMotion.test_vals = [-1.614165, 2.242648, -0.037218, 0.173751] #last 4 columns1112 pywrapper_rigidMotion.su2_exec = "mpirun -np 2 python launch_flatPlate_rigidMotion.py --parallel -f"1113 pywrapper_rigidMotion.timeout = 16001114 pywrapper_rigidMotion.tol = 0.000011115 pywrapper_rigidMotion.unsteady = True1116 test_list.append(pywrapper_rigidMotion)1117 ##############################################1118 ### Method of Manufactured Solutions (MMS) ###1119 ##############################################1120 # FVM, compressible, laminar N-S1121 mms_fvm_ns = TestCase('mms_fvm_ns')1122 mms_fvm_ns.cfg_dir = "mms/fvm_navierstokes"1123 mms_fvm_ns.cfg_file = "lam_mms_roe.cfg"1124 mms_fvm_ns.test_iter = 201125 mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000] #last 4 columns1126 mms_fvm_ns.su2_exec = "mpirun -n 2 SU2_CFD"1127 mms_fvm_ns.timeout = 16001128 mms_fvm_ns.tol = 0.00011129 test_list.append(mms_fvm_ns)1130 # FVM, incompressible, euler1131 mms_fvm_inc_euler = TestCase('mms_fvm_inc_euler')1132 mms_fvm_inc_euler.cfg_dir = "mms/fvm_incomp_euler"1133 mms_fvm_inc_euler.cfg_file = "inv_mms_jst.cfg"1134 mms_fvm_inc_euler.test_iter = 201135 mms_fvm_inc_euler.test_vals = [-9.128515, -9.441740, 0.000000, 0.000000] #last 4 columns1136 mms_fvm_inc_euler.su2_exec = "mpirun -np 2 SU2_CFD"1137 mms_fvm_inc_euler.timeout = 16001138 mms_fvm_inc_euler.tol = 0.00011139 test_list.append(mms_fvm_inc_euler)1140 # FVM, incompressible, laminar N-S1141 mms_fvm_inc_ns = TestCase('mms_fvm_inc_ns')1142 mms_fvm_inc_ns.cfg_dir = "mms/fvm_incomp_navierstokes"1143 mms_fvm_inc_ns.cfg_file = "lam_mms_fds.cfg"1144 mms_fvm_inc_ns.test_iter = 201145 mms_fvm_inc_ns.test_vals = [-7.414944, -7.631546, 0.000000, 0.000000] #last 4 columns1146 mms_fvm_inc_ns.su2_exec = "mpirun -np 2 SU2_CFD"1147 mms_fvm_inc_ns.timeout = 16001148 mms_fvm_inc_ns.tol = 0.00011149 test_list.append(mms_fvm_inc_ns)1150 # DG, compressible, euler1151 ringleb_dg_euler = TestCase('ringleb_dg_euler')1152 ringleb_dg_euler.cfg_dir = "mms/dg_ringleb"1153 ringleb_dg_euler.cfg_file = "ringleb_dg.cfg"1154 ringleb_dg_euler.test_iter = 1001155 ringleb_dg_euler.test_vals = [-5.136652, -4.724941, 0.000000, 0.000000] #last 4 columns1156 ringleb_dg_euler.su2_exec = "SU2_CFD"1157 ringleb_dg_euler.timeout = 16001158 ringleb_dg_euler.tol = 0.00011159 test_list.append(ringleb_dg_euler)1160 # DG, compressible, laminar N-S1161 mms_dg_ns = TestCase('mms_dg_ns')1162 mms_dg_ns.cfg_dir = "mms/dg_navierstokes"1163 mms_dg_ns.cfg_file = "lam_mms_dg.cfg"1164 mms_dg_ns.test_iter = 1001165 mms_dg_ns.test_vals = [-1.845393, 3.520699, 0.000000, 0.000000] #last 4 columns1166 mms_dg_ns.su2_exec = "SU2_CFD"1167 mms_dg_ns.timeout = 16001168 mms_dg_ns.tol = 0.00011169 test_list.append(mms_dg_ns)1170 # DG, compressible, laminar N-S 3D1171 mms_dg_ns_3d = TestCase('mms_dg_ns_3d')1172 mms_dg_ns_3d.cfg_dir = "mms/dg_navierstokes_3d"1173 mms_dg_ns_3d.cfg_file = "lam_mms_dg_3d.cfg"1174 mms_dg_ns_3d.test_iter = 1001175 mms_dg_ns_3d.test_vals = [-0.146826, 5.356413, 0.000000, 0.000000] #last 4 columns1176 mms_dg_ns_3d.su2_exec = "SU2_CFD"1177 mms_dg_ns_3d.timeout = 16001178 mms_dg_ns_3d.tol = 0.00011179 test_list.append(mms_dg_ns_3d)1180 ######################################1181 ### RUN TESTS ###1182 ######################################1183 pass_list = [ test.run_test() for test in test_list ]1184 ######################################1185 ### RUN SU2_SOL TESTS ###1186 ######################################1187 # parallel STL output using1188 stl_writer_test = TestCase('stl_writer_test')1189 stl_writer_test.cfg_dir = "rans/oneram6"1190 stl_writer_test.cfg_file = "turb_ONERAM6.cfg"1191 stl_writer_test.test_iter = 11192 stl_writer_test.su2_exec = "mpirun -n 2 SU2_SOL"1193 stl_writer_test.timeout = 16001194 stl_writer_test.reference_file = "surface_flow.stl.ref"1195 stl_writer_test.test_file = "surface_flow.stl"1196 pass_list.append(stl_writer_test.run_filediff())1197 test_list.append(stl_writer_test)1198 ######################################1199 ### RUN SU2_DEF TESTS ###1200 ######################################1201 # Inviscid NACA0012 (triangles)1202 naca0012_def = TestCase('naca0012_def')1203 naca0012_def.cfg_dir = "deformation/naca0012"1204 naca0012_def.cfg_file = "def_NACA0012.cfg"1205 naca0012_def.test_iter = 101206 naca0012_def.test_vals = [0.00354532] #residual1207 naca0012_def.su2_exec = "mpirun -n 2 SU2_DEF"1208 naca0012_def.timeout = 16001209 naca0012_def.tol = 1e-81210 pass_list.append(naca0012_def.run_def())1211 test_list.append(naca0012_def)1212 # Inviscid NACA0012 based on SURFACE_FILE input (surface_bump.dat)1213 naca0012_def_file = TestCase('naca0012_def_file')1214 naca0012_def_file.cfg_dir = "deformation/naca0012"1215 naca0012_def_file.cfg_file = "surface_file_NACA0012.cfg"1216 naca0012_def_file.test_iter = 101217 naca0012_def_file.test_vals = [0.00354532] #residual1218 naca0012_def_file.su2_exec = "mpirun -n 2 SU2_DEF"1219 naca0012_def_file.timeout = 16001220 naca0012_def_file.tol = 1e-81221 pass_list.append(naca0012_def_file.run_def())1222 test_list.append(naca0012_def_file)1223 # RAE2822 (mixed tris + quads)1224 rae2822_def = TestCase('rae2822_def')1225 rae2822_def.cfg_dir = "deformation/rae2822"1226 rae2822_def.cfg_file = "def_RAE2822.cfg"1227 rae2822_def.test_iter = 101228 rae2822_def.test_vals = [8.2438e-09] #residual1229 rae2822_def.su2_exec = "mpirun -n 2 SU2_DEF"1230 rae2822_def.timeout = 16001231 rae2822_def.tol = 1e-131232 pass_list.append(rae2822_def.run_def())1233 test_list.append(rae2822_def)1234 # Turb NACA4412 (quads, wall distance)1235 naca4412_def = TestCase('naca4412_def')1236 naca4412_def.cfg_dir = "deformation/naca4412"1237 naca4412_def.cfg_file = "def_NACA4412.cfg"1238 naca4412_def.test_iter = 101239 naca4412_def.test_vals = [2.210380e-12] #residual1240 naca4412_def.su2_exec = "mpirun -n 2 SU2_DEF"1241 naca4412_def.timeout = 16001242 naca4412_def.tol = 1e-121243 pass_list.append(naca4412_def.run_def())1244 test_list.append(naca4412_def)1245 # Brick of tets (inverse volume)1246 brick_tets_def = TestCase('brick_tets_def')1247 brick_tets_def.cfg_dir = "deformation/brick_tets"1248 brick_tets_def.cfg_file = "def_brick_tets.cfg"1249 brick_tets_def.test_iter = 101250 brick_tets_def.test_vals = [0.000954604] #residual1251 brick_tets_def.su2_exec = "mpirun -n 2 SU2_DEF"1252 brick_tets_def.timeout = 16001253 brick_tets_def.tol = 1e-91254 pass_list.append(brick_tets_def.run_def())1255 test_list.append(brick_tets_def)1256 # Brick of isotropic hexas (inverse volume)1257 brick_hex_def = TestCase('brick_hex_def')1258 brick_hex_def.cfg_dir = "deformation/brick_hex"1259 brick_hex_def.cfg_file = "def_brick_hex.cfg"1260 brick_hex_def.test_iter = 101261 brick_hex_def.test_vals = [0.000199532] #residual1262 brick_hex_def.su2_exec = "mpirun -n 2 SU2_DEF"1263 brick_hex_def.timeout = 16001264 brick_hex_def.tol = 1e-91265 pass_list.append(brick_hex_def.run_def())1266 test_list.append(brick_hex_def)1267 # Brick with a pyramid layer (inverse volume)1268 brick_pyra_def = TestCase('brick_pyra_def')1269 brick_pyra_def.cfg_dir = "deformation/brick_pyra"1270 brick_pyra_def.cfg_file = "def_brick_pyra.cfg"1271 brick_pyra_def.test_iter = 101272 brick_pyra_def.test_vals = [0.00160022] #residual1273 brick_pyra_def.su2_exec = "mpirun -n 2 SU2_DEF"1274 brick_pyra_def.timeout = 16001275 brick_pyra_def.tol = 1e-81276 pass_list.append(brick_pyra_def.run_def())1277 test_list.append(brick_pyra_def)1278 # Brick of isotropic prisms (inverse volume)1279 brick_prism_def = TestCase('brick_prism_def')1280 brick_prism_def.cfg_dir = "deformation/brick_prism"1281 brick_prism_def.cfg_file = "def_brick_prism.cfg"1282 brick_prism_def.test_iter = 101283 brick_prism_def.test_vals = [0.00260853] #residual1284 brick_prism_def.su2_exec = "mpirun -n 2 SU2_DEF"1285 brick_prism_def.timeout = 16001286 brick_prism_def.tol = 1e-81287 pass_list.append(brick_prism_def.run_def())1288 test_list.append(brick_prism_def)1289 # Brick of prisms with high aspect ratio cells near the wall (wall distance)1290 brick_prism_rans_def = TestCase('brick_prism_rans_def')1291 brick_prism_rans_def.cfg_dir = "deformation/brick_prism_rans"1292 brick_prism_rans_def.cfg_file = "def_brick_prism_rans.cfg"1293 brick_prism_rans_def.test_iter = 101294 brick_prism_rans_def.test_vals = [3.10348e-07] #residual1295 brick_prism_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"1296 brick_prism_rans_def.timeout = 16001297 brick_prism_rans_def.tol = 1e-121298 pass_list.append(brick_prism_rans_def.run_def())1299 test_list.append(brick_prism_rans_def)1300 # Brick of hexas with high aspect ratio cells near the wall (inverse volume)1301 brick_hex_rans_def = TestCase('brick_hex_rans_def')1302 brick_hex_rans_def.cfg_dir = "deformation/brick_hex_rans"1303 brick_hex_rans_def.cfg_file = "def_brick_hex_rans.cfg"1304 brick_hex_rans_def.test_iter = 101305 brick_hex_rans_def.test_vals = [3.55635e-06] #residual1306 brick_hex_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"1307 brick_hex_rans_def.timeout = 16001308 brick_hex_rans_def.tol = 1e-111309 pass_list.append(brick_hex_rans_def.run_def())1310 test_list.append(brick_hex_rans_def)1311 # Cylindrical FFD test1312 cylinder_ffd_def = TestCase('cylinder_ffd_def')1313 cylinder_ffd_def.cfg_dir = "deformation/cylindrical_ffd"1314 cylinder_ffd_def.cfg_file = "def_cylindrical.cfg"1315 cylinder_ffd_def.test_iter = 101316 cylinder_ffd_def.test_vals = [0.00054847] #residual1317 cylinder_ffd_def.su2_exec = "mpirun -n 2 SU2_DEF"1318 cylinder_ffd_def.timeout = 16001319 cylinder_ffd_def.tol = 1e-91320 pass_list.append(cylinder_ffd_def.run_def())1321 test_list.append(cylinder_ffd_def)1322 # Spherical FFD test1323 sphere_ffd_def = TestCase('sphere_ffd_def')1324 sphere_ffd_def.cfg_dir = "deformation/spherical_ffd"1325 sphere_ffd_def.cfg_file = "def_spherical.cfg"1326 sphere_ffd_def.test_iter = 101327 sphere_ffd_def.test_vals = [0.00359947] #residual1328 sphere_ffd_def.su2_exec = "mpirun -n 2 SU2_DEF"1329 sphere_ffd_def.timeout = 16001330 sphere_ffd_def.tol = 1e-81331 pass_list.append(sphere_ffd_def.run_def())1332 test_list.append(sphere_ffd_def)1333 # Spherical FFD test using BSplines1334 sphere_ffd_def_bspline = TestCase('sphere_ffd_def_bspline')1335 sphere_ffd_def_bspline.cfg_dir = "deformation/spherical_ffd"1336 sphere_ffd_def_bspline.cfg_file = "def_spherical_bspline.cfg"1337 sphere_ffd_def_bspline.test_iter = 101338 sphere_ffd_def_bspline.test_vals = [0.00208206] #residual1339 sphere_ffd_def_bspline.su2_exec = "mpirun -n 2 SU2_DEF"1340 sphere_ffd_def_bspline.timeout = 16001341 sphere_ffd_def_bspline.tol = 1e-81342 pass_list.append(sphere_ffd_def_bspline.run_def())1343 test_list.append(sphere_ffd_def_bspline)1344 # Tests summary1345 print('==================================================================')1346 print('Summary of the parallel tests')1347 print('python version:', sys.version)1348 for i, test in enumerate(test_list):1349 if (pass_list[i]):1350 print(' passed - %s'%test.tag)1351 else:1352 print('* FAILED - %s'%test.tag)1353 if all(pass_list):1354 sys.exit(0)1355 else:1356 sys.exit(1)1357 # done1358if __name__ == '__main__':...

Full Screen

Full Screen

hybrid_regression.py

Source:hybrid_regression.py Github

copy

Full Screen

1#!/usr/bin/env python2## \file parallel_regression.py3# \brief Python script for automated regression testing of SU2 examples4# \author A. Aranake, A. Campos, T. Economon, T. Lukaczyk, S. Padron5# \version 7.0.6 "Blackbird"6#7# SU2 Project Website: https://su2code.github.io8#9# The SU2 Project is maintained by the SU2 Foundation10# (http://su2foundation.org)11#12# Copyright 2012-2020, SU2 Contributors (cf. AUTHORS.md)13#14# SU2 is free software; you can redistribute it and/or15# modify it under the terms of the GNU Lesser General Public16# License as published by the Free Software Foundation; either17# version 2.1 of the License, or (at your option) any later version.18#19# SU2 is distributed in the hope that it will be useful,20# but WITHOUT ANY WARRANTY; without even the implied warranty of21# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU22# Lesser General Public License for more details.23#24# You should have received a copy of the GNU Lesser General Public25# License along with SU2. If not, see <http://www.gnu.org/licenses/>.26# make print(*args) function available in PY2.6+, does'nt work on PY < 2.627from __future__ import print_function28import sys29from TestCase import TestCase30def main():31 '''This program runs SU2 and ensures that the output matches specified values.32 This will be used to do checks when code is pushed to github33 to make sure nothing is broken. '''34 test_list = []35 ##########################36 ### Compressible Euler ###37 ##########################38 # Channel39 channel = TestCase('channel')40 channel.cfg_dir = "euler/channel"41 channel.cfg_file = "inv_channel_RK.cfg"42 channel.test_iter = 2043 channel.test_vals = [-2.667326, 2.797439, 0.018717, 0.006906]44 test_list.append(channel)45 # NACA001246 naca0012 = TestCase('naca0012')47 naca0012.cfg_dir = "euler/naca0012"48 naca0012.cfg_file = "inv_NACA0012_Roe.cfg"49 naca0012.test_iter = 2050 naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217]51 test_list.append(naca0012)52 # Supersonic wedge53 wedge = TestCase('wedge')54 wedge.cfg_dir = "euler/wedge"55 wedge.cfg_file = "inv_wedge_HLLC.cfg"56 wedge.test_iter = 2057 wedge.test_vals = [-0.942862, 4.784581, -0.208106, 0.036665]58 test_list.append(wedge)59 # ONERA M6 Wing60 oneram6 = TestCase('oneram6')61 oneram6.cfg_dir = "euler/oneram6"62 oneram6.cfg_file = "inv_ONERAM6.cfg"63 oneram6.test_iter = 1064 oneram6.test_vals = [0.281704, 0.011821]65 test_list.append(oneram6)66 # Fixed CL NACA001267 fixedCL_naca0012 = TestCase('fixedcl_naca0012')68 fixedCL_naca0012.cfg_dir = "fixed_cl/naca0012"69 fixedCL_naca0012.cfg_file = "inv_NACA0012.cfg"70 fixedCL_naca0012.test_iter = 1071 fixedCL_naca0012.test_vals = [-12.130189, -6.702728, 0.300000, 0.019470]72 test_list.append(fixedCL_naca0012)73 # HYPERSONIC FLOW PAST BLUNT BODY74 bluntbody = TestCase('bluntbody')75 bluntbody.cfg_dir = "euler/bluntbody"76 bluntbody.cfg_file = "blunt.cfg"77 bluntbody.test_iter = 2078 bluntbody.test_vals = [0.540010, 6.916656, 0.000027, 1.869004]79 test_list.append(bluntbody)80 ##########################81 ### Compressible N-S ###82 ##########################83 # Laminar flat plate84 flatplate = TestCase('flatplate')85 flatplate.cfg_dir = "navierstokes/flatplate"86 flatplate.cfg_file = "lam_flatplate.cfg"87 flatplate.test_iter = 2088 flatplate.test_vals = [-4.680775, 0.781235, -0.135957, 0.022978]89 test_list.append(flatplate)90 # Laminar cylinder (steady)91 cylinder = TestCase('cylinder')92 cylinder.cfg_dir = "navierstokes/cylinder"93 cylinder.cfg_file = "lam_cylinder.cfg"94 cylinder.test_iter = 2595 cylinder.test_vals = [-6.765432, -1.297428, 0.019596, 0.310240]96 test_list.append(cylinder)97 # Laminar cylinder (low Mach correction)98 cylinder_lowmach = TestCase('cylinder_lowmach')99 cylinder_lowmach.cfg_dir = "navierstokes/cylinder"100 cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"101 cylinder_lowmach.test_iter = 25102 cylinder_lowmach.test_vals = [-6.850130, -1.388096, -0.056203, 108.140819]103 test_list.append(cylinder_lowmach)104 # 2D Poiseuille flow (body force driven with periodic inlet / outlet)105 poiseuille = TestCase('poiseuille')106 poiseuille.cfg_dir = "navierstokes/poiseuille"107 poiseuille.cfg_file = "lam_poiseuille.cfg"108 poiseuille.test_iter = 10109 poiseuille.test_vals = [-5.048282, 0.650814, 0.008714, 13.677678]110 test_list.append(poiseuille)111 # 2D Poiseuille flow (inlet profile file)112 poiseuille_profile = TestCase('poiseuille_profile')113 poiseuille_profile.cfg_dir = "navierstokes/poiseuille"114 poiseuille_profile.cfg_file = "profile_poiseuille.cfg"115 poiseuille_profile.test_iter = 10116 poiseuille_profile.test_vals = [-12.494721, -7.712408, -0.000000, 2.085796]117 test_list.append(poiseuille_profile)118 ##########################119 ### Compressible RANS ###120 ##########################121 # RAE2822 SA122 rae2822_sa = TestCase('rae2822_sa')123 rae2822_sa.cfg_dir = "rans/rae2822"124 rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"125 rae2822_sa.test_iter = 20126 rae2822_sa.test_vals = [-2.021218, -5.268447, 0.807465, 0.060897]127 test_list.append(rae2822_sa)128 # RAE2822 SST129 rae2822_sst = TestCase('rae2822_sst')130 rae2822_sst.cfg_dir = "rans/rae2822"131 rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"132 rae2822_sst.test_iter = 20133 rae2822_sst.test_vals = [-0.510637, 4.876603, 0.812485, 0.061969]134 test_list.append(rae2822_sst)135 # RAE2822 SST_SUST136 rae2822_sst_sust = TestCase('rae2822_sst_sust')137 rae2822_sst_sust.cfg_dir = "rans/rae2822"138 rae2822_sst_sust.cfg_file = "turb_SST_SUST_RAE2822.cfg"139 rae2822_sst_sust.test_iter = 20140 rae2822_sst_sust.test_vals = [-2.429813, 4.876602, 0.812485, 0.061969]141 test_list.append(rae2822_sst_sust)142 # Flat plate143 turb_flatplate = TestCase('turb_flatplate')144 turb_flatplate.cfg_dir = "rans/flatplate"145 turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"146 turb_flatplate.test_iter = 20147 turb_flatplate.test_vals = [-4.157169, -6.737133, -0.176253, 0.057446]148 test_list.append(turb_flatplate)149 # ONERA M6 Wing150 turb_oneram6 = TestCase('turb_oneram6')151 turb_oneram6.cfg_dir = "rans/oneram6"152 turb_oneram6.cfg_file = "turb_ONERAM6.cfg"153 turb_oneram6.test_iter = 10154 turb_oneram6.test_vals = [-2.412446, -6.702976, 0.229866, 0.147638]155 test_list.append(turb_oneram6)156 # NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)157 turb_naca0012_sa = TestCase('turb_naca0012_sa')158 turb_naca0012_sa.cfg_dir = "rans/naca0012"159 turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"160 turb_naca0012_sa.test_iter = 10161 turb_naca0012_sa.test_vals = [-12.076819, -16.049252, 1.064326, 0.019770]162 test_list.append(turb_naca0012_sa)163 # NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)164 turb_naca0012_sst = TestCase('turb_naca0012_sst')165 turb_naca0012_sst.cfg_dir = "rans/naca0012"166 turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"167 turb_naca0012_sst.test_iter = 10168 turb_naca0012_sst.test_vals = [-15.273728, -6.243783, 1.049988, 0.019165]169 test_list.append(turb_naca0012_sst)170 # NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)171 turb_naca0012_sst_sust = TestCase('turb_naca0012_sst_sust')172 turb_naca0012_sst_sust.cfg_dir = "rans/naca0012"173 turb_naca0012_sst_sust.cfg_file = "turb_NACA0012_sst_sust.cfg"174 turb_naca0012_sst_sust.test_iter = 10175 turb_naca0012_sst_sust.test_vals = [-14.851214, -6.062566, 1.005233, 0.019014]176 test_list.append(turb_naca0012_sst_sust)177 # PROPELLER178 propeller = TestCase('propeller')179 propeller.cfg_dir = "rans/propeller"180 propeller.cfg_file = "propeller.cfg"181 propeller.test_iter = 10182 propeller.test_vals = [-3.389576, -8.409529, 0.000048, 0.056329]183 test_list.append(propeller)184 #################################185 ## Compressible RANS Restart ###186 #################################187 # NACA0012 SST Multigrid restart188 turb_naca0012_sst_restart_mg = TestCase('turb_naca0012_sst_restart_mg')189 turb_naca0012_sst_restart_mg.cfg_dir = "rans/naca0012"190 turb_naca0012_sst_restart_mg.cfg_file = "turb_NACA0012_sst_multigrid_restart.cfg"191 turb_naca0012_sst_restart_mg.test_iter = 20192 turb_naca0012_sst_restart_mg.ntest_vals = 5193 turb_naca0012_sst_restart_mg.test_vals = [-7.653296, -7.729472, -1.981061, -0.000016, 0.079062]194 test_list.append(turb_naca0012_sst_restart_mg)195 #############################196 ### Compressibele RANS UQ ###197 #############################198 # NACA0012 1c199 turb_naca0012_1c = TestCase('turb_naca0012_1c')200 turb_naca0012_1c.cfg_dir = "rans_uq/naca0012"201 turb_naca0012_1c.cfg_file = "turb_NACA0012_uq_1c.cfg"202 turb_naca0012_1c.test_iter = 10203 turb_naca0012_1c.test_vals = [-4.979339, 1.140084, 1.217182, 0.220079]204 test_list.append(turb_naca0012_1c)205 # NACA0012 2c206 turb_naca0012_2c = TestCase('turb_naca0012_2c')207 turb_naca0012_2c.cfg_dir = "rans_uq/naca0012"208 turb_naca0012_2c.cfg_file = "turb_NACA0012_uq_2c.cfg"209 turb_naca0012_2c.test_iter = 10210 turb_naca0012_2c.test_vals = [-5.484195, 0.969780, 1.315926, 0.258346]211 test_list.append(turb_naca0012_2c)212 # NACA0012 3c213 turb_naca0012_3c = TestCase('turb_naca0012_3c')214 turb_naca0012_3c.cfg_dir = "rans_uq/naca0012"215 turb_naca0012_3c.cfg_file = "turb_NACA0012_uq_3c.cfg"216 turb_naca0012_3c.test_iter = 10217 turb_naca0012_3c.test_vals = [-5.586959, 0.932347, 1.540973, 0.345562]218 test_list.append(turb_naca0012_3c)219 # NACA0012 p1c1220 turb_naca0012_p1c1 = TestCase('turb_naca0012_p1c1')221 turb_naca0012_p1c1.cfg_dir = "rans_uq/naca0012"222 turb_naca0012_p1c1.cfg_file = "turb_NACA0012_uq_p1c1.cfg"223 turb_naca0012_p1c1.test_iter = 10224 turb_naca0012_p1c1.test_vals = [-5.132080, 1.076459, 1.183320, 0.207012]225 test_list.append(turb_naca0012_p1c1)226 # NACA0012 p1c2227 turb_naca0012_p1c2 = TestCase('turb_naca0012_p1c2')228 turb_naca0012_p1c2.cfg_dir = "rans_uq/naca0012"229 turb_naca0012_p1c2.cfg_file = "turb_NACA0012_uq_p1c2.cfg"230 turb_naca0012_p1c2.test_iter = 10231 turb_naca0012_p1c2.test_vals = [-5.556645, 0.945121, 1.246337, 0.231311]232 test_list.append(turb_naca0012_p1c2)233 ######################################234 ### Harmonic Balance ###235 ######################################236 # Description of the regression test237 harmonic_balance = TestCase('harmonic_balance')238 harmonic_balance.cfg_dir = "harmonic_balance"239 harmonic_balance.cfg_file = "HB.cfg"240 harmonic_balance.test_iter = 25241 harmonic_balance.test_vals = [-1.589755, 3.922207, 0.006725, 0.099455]242 harmonic_balance.new_output = False243 test_list.append(harmonic_balance)244 # Turbulent pitching NACA 64a010 airfoil245 hb_rans_preconditioning = TestCase('hb_rans_preconditioning')246 hb_rans_preconditioning.cfg_dir = "harmonic_balance/hb_rans_preconditioning"247 hb_rans_preconditioning.cfg_file = "davis.cfg"248 hb_rans_preconditioning.test_iter = 25249 hb_rans_preconditioning.test_vals = [-1.909633, -5.954752, 0.007773, 0.131217]250 hb_rans_preconditioning.new_output = False251 test_list.append(hb_rans_preconditioning)252 ######################################253 ### Moving Wall ###254 ######################################255 # Lid-driven cavity256 cavity = TestCase('cavity')257 cavity.cfg_dir = "moving_wall/cavity"258 cavity.cfg_file = "lam_cavity.cfg"259 cavity.test_iter = 25260 cavity.test_vals = [-5.627934, -0.164469, 0.051998, 2.547065]261 test_list.append(cavity)262 # Spinning cylinder263 spinning_cylinder = TestCase('spinning_cylinder')264 spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"265 spinning_cylinder.cfg_file = "spinning_cylinder.cfg"266 spinning_cylinder.test_iter = 25267 spinning_cylinder.test_vals = [-7.996313, -2.601764, 1.510692, 1.493876]268 test_list.append(spinning_cylinder)269 ######################################270 ### Unsteady ###271 ######################################272 # Square cylinder273 square_cylinder = TestCase('square_cylinder')274 square_cylinder.cfg_dir = "unsteady/square_cylinder"275 square_cylinder.cfg_file = "turb_square.cfg"276 square_cylinder.test_iter = 3277 square_cylinder.test_vals = [-1.162572, 0.066371, 1.399790, 2.220393]278 square_cylinder.unsteady = True279 test_list.append(square_cylinder)280 # Gust281 sine_gust = TestCase('sine_gust')282 sine_gust.cfg_dir = "gust"283 sine_gust.cfg_file = "inv_gust_NACA0012.cfg"284 sine_gust.test_iter = 5285 sine_gust.test_vals = [-1.977520, 3.481804, -0.012404, -0.007452]286 sine_gust.unsteady = True287 test_list.append(sine_gust)288 # Aeroelastic289 aeroelastic = TestCase('aeroelastic')290 aeroelastic.cfg_dir = "aeroelastic"291 aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"292 aeroelastic.test_iter = 2293 aeroelastic.test_vals = [0.074525, 0.033127, -0.001650, -0.000127]294 aeroelastic.unsteady = True295 test_list.append(aeroelastic)296 # Delayed Detached Eddy Simulation297 ddes_flatplate = TestCase('ddes_flatplate')298 ddes_flatplate.cfg_dir = "ddes/flatplate"299 ddes_flatplate.cfg_file = "ddes_flatplate.cfg"300 ddes_flatplate.test_iter = 10301 ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783]302 ddes_flatplate.unsteady = True303 test_list.append(ddes_flatplate)304 ######################################305 ### NICFD ###306 ######################################307 # Rarefaction shock wave edge_VW308 edge_VW = TestCase('edge_VW')309 edge_VW.cfg_dir = "nicf/edge"310 edge_VW.cfg_file = "edge_VW.cfg"311 edge_VW.test_iter = 100312 edge_VW.test_vals = [-5.040283, 1.124491, -0.000009, 0.000000]313 test_list.append(edge_VW)314 # Rarefaction shock wave edge_PPR315 edge_PPR = TestCase('edge_PPR')316 edge_PPR.cfg_dir = "nicf/edge"317 edge_PPR.cfg_file = "edge_PPR.cfg"318 edge_PPR.test_iter = 100319 edge_PPR.test_vals = [-5.401640, 0.738165, -0.000035, 0.000000]320 test_list.append(edge_PPR)321 ######################################322 ### Turbomachinery ###323 ######################################324 # Jones APU Turbocharger325 Jones_tc = TestCase('jones_turbocharger')326 Jones_tc.cfg_dir = "turbomachinery/APU_turbocharger"327 Jones_tc.cfg_file = "Jones.cfg"328 Jones_tc.test_iter = 5329 Jones_tc.test_vals = [-5.280316, 0.379651, 44.725470, 2.271540]330 Jones_tc.new_output = False331 test_list.append(Jones_tc)332 # Jones APU Turbocharger restart333 Jones_tc_rst = TestCase('jones_turbocharger_restart')334 Jones_tc_rst.cfg_dir = "turbomachinery/APU_turbocharger"335 Jones_tc_rst.cfg_file = "Jones_rst.cfg"336 Jones_tc_rst.test_iter = 5337 Jones_tc_rst.test_vals = [-4.626647, -1.570858, 34.014100, 10.190720]338 Jones_tc_rst.new_output = False339 test_list.append(Jones_tc_rst)340 # 2D axial stage341 axial_stage2D = TestCase('axial_stage2D')342 axial_stage2D.cfg_dir = "turbomachinery/axial_stage_2D"343 axial_stage2D.cfg_file = "Axial_stage2D.cfg"344 axial_stage2D.test_iter = 20345 axial_stage2D.test_vals = [-1.933199, 5.381560, 73.357900, 1.780500]346 axial_stage2D.new_output = False347 test_list.append(axial_stage2D)348 # 2D transonic stator349 transonic_stator = TestCase('transonic_stator')350 transonic_stator.cfg_dir = "turbomachinery/transonic_stator_2D"351 transonic_stator.cfg_file = "transonic_stator.cfg"352 transonic_stator.test_iter = 20353 transonic_stator.test_vals = [-0.563540, 5.823232, 96.736080, 0.062426]354 transonic_stator.new_output = False355 test_list.append(transonic_stator)356 # 2D transonic stator restart357 transonic_stator_rst = TestCase('transonic_stator_restart')358 transonic_stator_rst.cfg_dir = "turbomachinery/transonic_stator_2D"359 transonic_stator_rst.cfg_file = "transonic_stator_rst.cfg"360 transonic_stator_rst.test_iter = 20361 transonic_stator_rst.test_vals = [-6.621626, -0.614379, 5.002986, 0.002951]362 transonic_stator_rst.new_output = False363 test_list.append(transonic_stator_rst)364 ######################################365 ### Sliding Mesh ###366 ######################################367 # Uniform flow368 uniform_flow = TestCase('uniform_flow')369 uniform_flow.cfg_dir = "sliding_interface/uniform_flow"370 uniform_flow.cfg_file = "uniform_NN.cfg"371 uniform_flow.test_iter = 5372 uniform_flow.test_vals = [5.000000, 0.000000, -0.188748, -10.631530]373 uniform_flow.unsteady = True374 uniform_flow.multizone = True375 test_list.append(uniform_flow)376 # Channel_2D377 channel_2D = TestCase('channel_2D')378 channel_2D.cfg_dir = "sliding_interface/channel_2D"379 channel_2D.cfg_file = "channel_2D_WA.cfg"380 channel_2D.test_iter = 2381 channel_2D.test_vals = [2.000000, 0.000000, 0.398089, 0.352762, 0.405397]382 channel_2D.unsteady = True383 channel_2D.multizone = True384 test_list.append(channel_2D)385 # Channel_3D386 channel_3D = TestCase('channel_3D')387 channel_3D.cfg_dir = "sliding_interface/channel_3D"388 channel_3D.cfg_file = "channel_3D_WA.cfg"389 channel_3D.test_iter = 2390 channel_3D.test_vals = [2.000000, 0.000000, 0.620151, 0.505157, 0.415249]391 channel_3D.unsteady = True392 channel_3D.multizone = True393 test_list.append(channel_3D)394 # Pipe395 pipe = TestCase('pipe')396 pipe.cfg_dir = "sliding_interface/pipe"397 pipe.cfg_file = "pipe_NN.cfg"398 pipe.test_iter = 2399 pipe.test_vals = [0.150024, 0.491949, 0.677757, 0.963990, 1.006944]400 pipe.unsteady = True401 pipe.multizone = True402 test_list.append(pipe)403 # Rotating cylinders404 rotating_cylinders = TestCase('rotating_cylinders')405 rotating_cylinders.cfg_dir = "sliding_interface/rotating_cylinders"406 rotating_cylinders.cfg_file = "rot_cylinders_WA.cfg"407 rotating_cylinders.test_iter = 3408 rotating_cylinders.test_vals = [3.000000, 0.000000, 0.777567, 1.134807, 1.224136]409 rotating_cylinders.unsteady = True410 rotating_cylinders.multizone = True411 test_list.append(rotating_cylinders)412 # Supersonic vortex shedding413 supersonic_vortex_shedding = TestCase('supersonic_vortex_shedding')414 supersonic_vortex_shedding.cfg_dir = "sliding_interface/supersonic_vortex_shedding"415 supersonic_vortex_shedding.cfg_file = "sup_vor_shed_WA.cfg"416 supersonic_vortex_shedding.test_iter = 5417 supersonic_vortex_shedding.test_vals = [5.000000, 0.000000, 1.216554, 1.639121]418 supersonic_vortex_shedding.unsteady = True419 supersonic_vortex_shedding.multizone = True420 test_list.append(supersonic_vortex_shedding)421 # Bars_SST_2D422 bars_SST_2D = TestCase('bars_SST_2D')423 bars_SST_2D.cfg_dir = "sliding_interface/bars_SST_2D"424 bars_SST_2D.cfg_file = "bars.cfg"425 bars_SST_2D.test_iter = 13426 bars_SST_2D.test_vals = [13.000000, -0.619179, -1.564701]427 bars_SST_2D.multizone = True428 test_list.append(bars_SST_2D)429 ##########################430 ### FEA - FSI ###431 ##########################432 # Static beam, 3d433 statbeam3d = TestCase('statbeam3d')434 statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"435 statbeam3d.cfg_file = "configBeam_3d.cfg"436 statbeam3d.test_iter = 0437 statbeam3d.test_vals = [-2.378370, -1.585252, -2.028505, 6.4359e+04]438 test_list.append(statbeam3d)439 # Dynamic beam, 2d440 dynbeam2d = TestCase('dynbeam2d')441 dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"442 dynbeam2d.cfg_file = "configBeam_2d.cfg"443 dynbeam2d.test_iter = 6444 dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 66127.000000]445 dynbeam2d.unsteady = True446 test_list.append(dynbeam2d)447 # FSI, 2d448 fsi2d = TestCase('fsi2d')449 fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"450 fsi2d.cfg_file = "configFSI.cfg"451 fsi2d.test_iter = 4452 fsi2d.test_vals = [4.000000, 0.000000, -3.764089, -4.081119]453 fsi2d.multizone= True454 fsi2d.unsteady = True455 test_list.append(fsi2d)456 # FSI, Static, 2D, new mesh solver457 stat_fsi = TestCase('stat_fsi')458 stat_fsi.cfg_dir = "fea_fsi/stat_fsi"459 stat_fsi.cfg_file = "config.cfg"460 stat_fsi.test_iter = 7461 stat_fsi.test_vals = [-3.242834, -4.866608, 0.000000, 11.000000]462 stat_fsi.multizone = True463 test_list.append(stat_fsi)464 # FSI, Dynamic, 2D, new mesh solver465 dyn_fsi = TestCase('dyn_fsi')466 dyn_fsi.cfg_dir = "fea_fsi/dyn_fsi"467 dyn_fsi.cfg_file = "config.cfg"468 dyn_fsi.test_iter = 4469 dyn_fsi.test_vals = [-4.379823, -4.005990, 0.000000, 74.000000]470 dyn_fsi.multizone = True471 dyn_fsi.unsteady = True472 test_list.append(dyn_fsi)473 # FSI, Static, 2D, new mesh solver, restart474 stat_fsi_restart = TestCase('stat_fsi_restart')475 stat_fsi_restart.cfg_dir = "fea_fsi/stat_fsi"476 stat_fsi_restart.cfg_file = "config_restart.cfg"477 stat_fsi_restart.test_iter = 1478 stat_fsi_restart.test_vals = [-3.474239, -4.250710, 0.000000, 36.000000]479 stat_fsi_restart.multizone = True480 test_list.append(stat_fsi_restart)481 ##############################################482 ### Method of Manufactured Solutions (MMS) ###483 ##############################################484 # FVM, compressible, laminar N-S485 mms_fvm_ns = TestCase('mms_fvm_ns')486 mms_fvm_ns.cfg_dir = "mms/fvm_navierstokes"487 mms_fvm_ns.cfg_file = "lam_mms_roe.cfg"488 mms_fvm_ns.test_iter = 20489 mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000]490 test_list.append(mms_fvm_ns)491 ######################################492 ### RUN TESTS ###493 ######################################494 for test in test_list:495 test.su2_exec = "SU2_CFD -t 2"496 test.timeout = 600497 test.tol = 1e-4498 #end499 pass_list = [ test.run_test() for test in test_list ]500 # Tests summary501 print('==================================================================')502 print('Summary of the parallel tests')503 print('python version:', sys.version)504 for i, test in enumerate(test_list):505 if (pass_list[i]):506 print(' passed - %s'%test.tag)507 else:508 print('* FAILED - %s'%test.tag)509 if all(pass_list):510 sys.exit(0)511 else:512 sys.exit(1)513 # done514if __name__ == '__main__':...

Full Screen

Full Screen

parselog.py

Source:parselog.py Github

copy

Full Screen

1import os2import pylab3import sys4log_file = sys.argv[1]5train_iter = []6train_loss = []7test_iter = []8test_acc = []9test_loss = []10class CaffeVersion:11 OLD, NEW = range(0, 2)12CAFFE_VERSION = CaffeVersion.NEW13# prefix_loss = (CAFFE_VERSION is CaffeVersion.OLD) and 'loss = ' or 'loss = '14prefix_loss = (CAFFE_VERSION is CaffeVersion.OLD) and 'flow_loss0 = ' or 'flow_loss0 = '15prefix_acc = 'accuracy_texture = '16prefix_iter = 'Iteration '17# prefix_scr0 = 'Test score #0: '18# prefix_scr1 = 'Test score #1: '19prefix_train_scr0 = 'Train net output #0: flow_loss0 = '20prefix_scr0 = 'Test net output #0: flow_loss0 = '21prefix_scr1 = 'Test net output #1: '22plateau = 423with open(log_file) as f:24 for line in f:25 if line.find(prefix_iter) >= 0:26 st = line.find(prefix_iter) + len(prefix_iter)27 ed = line.find(',')28 iter_num = int(line[st:ed])29 if line.find('Testing net') >= 0:30 test_iter.append(iter_num)31 else:32 if line.find('lr = ') < 0:33 train_iter.append(iter_num)34 if CAFFE_VERSION is CaffeVersion.OLD:35 if line.find(prefix_train_scr0) >= 0:36 # st = line.find(prefix_loss) + len(prefix_loss)37 st = line.find(prefix_train_scr0) + len(prefix_train_scr0)38 train_loss.append(float(line[st:]))39 continue40 if line.find(prefix_scr0) >= 0:41 st = line.find(prefix_scr0) + len(prefix_scr0)42 test_acc.append(float(line[st:]))43 continue44 if line.find(prefix_scr1) >= 0:45 st = line.find(prefix_scr1) + len(prefix_scr1)46 test_loss.append(float(line[st:]))47 continue48 else:49 if line.find(prefix_train_scr0) >= 0:50 st = line.find(prefix_train_scr0) + len(prefix_train_scr0)51 ed = line.find('(*')52 loss = float(line[st:ed])53 if loss > plateau:54 loss = plateau55 if line.find('flow_loss0 =') >= 0:56 train_loss.append(loss)57 if line.find('Test net') >= 0:58 test_loss.append(loss)59 continue60 if line.find(prefix_scr0) >= 0:61 st = line.find(prefix_scr0) + len(prefix_scr0)62 ed = line.find('(*')63 loss = float(line[st:ed])64 if line.find('flow_loss0 =') >= 0:65 test_loss.append(loss)66 continue67 if line.find(prefix_acc) >= 0 and line.find('Test net') >= 0:68 st = line.find(prefix_acc) + len(prefix_acc)69 test_acc.append(float(line[st:]))70 continue71if len(train_iter) - len(train_loss) == 1:72 train_iter = train_iter[:-1]73if len(train_iter) - len(train_loss) == 2:74 train_iter = train_iter[:-2]75if len(test_iter) - len(test_loss) == 1:76 test_iter = test_iter[:-1]77print len(train_iter), len(train_loss)78print len(test_iter), len(test_loss)79if len(train_iter) > 100:80 pylab.plot(train_iter[4:len(train_iter)], train_loss[4:len(train_loss)])81 pylab.plot(test_iter[1:len(test_iter)], test_loss[1:len(test_iter)], 'r')82else:83 pylab.plot(train_iter[4:len(train_iter)], train_loss[4:len(train_loss)],'*-')84 pylab.plot(test_iter[1:len(test_iter)], test_loss[1:len(test_iter)], 'rs-')85pylab.plot(train_iter, train_loss, 'b')86pylab.plot(test_iter, test_loss, 'r')87pylab.legend(['training', 'testing'])88pylab.xlabel('iter'), pylab.ylabel('loss')89# pylab.figure()90# pylab.plot(test_iter, test_acc)91# pylab.xlabel('iter'), pylab.ylabel('test accuracy')...

Full Screen

Full Screen

test1.py

Source:test1.py Github

copy

Full Screen

1# coding=utf-82# test_list = [1, 2, 3, 4]3#4# test_iter = iter(test_list)5#6# print(next(test_iter))7# print(next(test_iter))8# print(test_iter.__next__())9# print(test_iter.__next__())10# print(test_iter.__next__())11# When we reach the end and there is no more data to be returned,12# it will raise StopIteration.13# raise StopIteration14# next(test_iter)15# # 手动实现for loop16# test_list_two = ["123", "456", "789"]17# for item in test_list_two:18# print(item)19# # for loop 的大致原理20# # a for loop takes an iterator and iterates over it using next()21# test_iter = iter(test_list_two)22# while True:23# try:24# print(next(test_iter))25# except StopIteration:26# break27# next和iter也只不过是调用的实例的self.__next__,和self.__iter__而已28# # 至于for loop的内部原理是不是这样呢?我们可以做一个实验29# class TestIterator:30# def __init__(self, max):31# self.max = max32#33# def __iter__(self):34# self.n = 035# return self36#37# def __next__(self):38# if self.n < self.max:39# result = 3 ** self.n40# self.n += 141# return result42# else:43# raise StopIteration44#45#46# a = TestIterator(4)47#48# for item in a:49# print(item)50# 不过要小心,因为循环使用的无限续循环,迭代对象很有可能永远了无法耗尽51# 如下面的例子,int()是可迭代的,然后iter()方法里面第二个参数是哨兵52# 意思就是如果next值不是第二个参数,就继续迭代53# test_iter = iter(int, 1)54# print(test_iter.__next__())55# print(test_iter.__next__())56# print(test_iter.__next__())57# print(test_iter.__next__())58# print(test_iter.__next__())59# print(test_iter.__next__())60# print(test_iter.__next__())61# print(test_iter.__next__())62# print(test_iter.__next__())63#64# 我们也可以手动让for循环无线循环,只要raise StopIteration就行了65class TestIteratorTwo:66 def __iter__(self):67 self.num = 168 return self69 def __next__(self):70 num = self.num71 print(num)72 self.num += 273 return num74# 这样就无限循环了,看吧,即使是for循环里面pass了,也是有输出的75for item in TestIteratorTwo():...

Full Screen

Full Screen

Automation Testing Tutorials

Learn to execute automation testing from scratch with LambdaTest Learning Hub. Right from setting up the prerequisites to run your first automation test, to following best practices and diving deeper into advanced test scenarios. LambdaTest Learning Hubs compile a list of step-by-step guides to help you be proficient with different test automation frameworks i.e. Selenium, Cypress, TestNG etc.

LambdaTest Learning Hubs:

YouTube

You could also refer to video tutorials over LambdaTest YouTube channel to get step by step demonstration from industry experts.

Run yandex-tank automation tests on LambdaTest cloud grid

Perform automation testing on 3000+ real desktop and mobile devices online.

Try LambdaTest Now !!

Get 100 minutes of automation test minutes FREE!!

Next-Gen App & Browser Testing Cloud

Was this article helpful?

Helpful

NotHelpful