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Updating regression values.
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Lines changed: 188 additions & 188 deletions

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‎TestCases/hybrid_regression.py‎

Lines changed: 33 additions & 33 deletions
Original file line numberDiff line numberDiff line change
@@ -6,8 +6,8 @@
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# \version 7.0.5 "Blackbird"
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#
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# SU2 Project Website: https://su2code.github.io
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#
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# The SU2 Project is maintained by the SU2 Foundation
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#
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# The SU2 Project is maintained by the SU2 Foundation
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# (http://su2foundation.org)
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#
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# Copyright 2012-2020, SU2 Contributors (cf. AUTHORS.md)
@@ -16,7 +16,7 @@
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# modify it under the terms of the GNU Lesser General Public
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# License as published by the Free Software Foundation; either
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# version 2.1 of the License, or (at your option) any later version.
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#
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#
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# SU2 is distributed in the hope that it will be useful,
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# but WITHOUT ANY WARRANTY; without even the implied warranty of
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# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
@@ -29,11 +29,11 @@
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from __future__ import print_function
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import sys
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from TestCase import TestCase
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from TestCase import TestCase
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def main():
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'''This program runs SU2 and ensures that the output matches specified values.
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This will be used to do checks when code is pushed to github
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'''This program runs SU2 and ensures that the output matches specified values.
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This will be used to do checks when code is pushed to github
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to make sure nothing is broken. '''
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test_list = []
@@ -50,15 +50,15 @@ def main():
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channel.test_vals = [-2.667326, 2.797439, 0.018717, 0.006906]
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test_list.append(channel)
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# NACA0012
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# NACA0012
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naca0012 = TestCase('naca0012')
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naca0012.cfg_dir = "euler/naca0012"
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naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
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naca0012.test_iter = 20
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naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217]
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test_list.append(naca0012)
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# Supersonic wedge
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# Supersonic wedge
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wedge = TestCase('wedge')
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wedge.cfg_dir = "euler/wedge"
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wedge.cfg_file = "inv_wedge_HLLC.cfg"
@@ -82,7 +82,7 @@ def main():
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fixedCL_naca0012.test_vals = [-12.130189, -6.702728, 0.300000, 0.019470]
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test_list.append(fixedCL_naca0012)
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85-
# HYPERSONIC FLOW PAST BLUNT BODY
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# HYPERSONIC FLOW PAST BLUNT BODY
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bluntbody = TestCase('bluntbody')
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bluntbody.cfg_dir = "euler/bluntbody"
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bluntbody.cfg_file = "blunt.cfg"
@@ -145,7 +145,7 @@ def main():
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rae2822_sa.test_iter = 20
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rae2822_sa.test_vals = [-2.021218, -5.268447, 0.807465, 0.060897]
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test_list.append(rae2822_sa)
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# RAE2822 SST
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rae2822_sst = TestCase('rae2822_sst')
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rae2822_sst.cfg_dir = "rans/rae2822"
@@ -185,7 +185,7 @@ def main():
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turb_naca0012_sa.test_iter = 10
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turb_naca0012_sa.test_vals = [-12.076819, -16.049252, 1.064326, 0.019770]
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test_list.append(turb_naca0012_sa)
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# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
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turb_naca0012_sst = TestCase('turb_naca0012_sst')
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turb_naca0012_sst.cfg_dir = "rans/naca0012"
@@ -209,11 +209,11 @@ def main():
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propeller.test_iter = 10
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propeller.test_vals = [-3.389576, -8.409529, 0.000048, 0.056329]
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test_list.append(propeller)
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#################################
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## Compressible RANS Restart ###
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#################################
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# NACA0012 SST Multigrid restart
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turb_naca0012_sst_restart_mg = TestCase('turb_naca0012_sst_restart_mg')
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turb_naca0012_sst_restart_mg.cfg_dir = "rans/naca0012"
@@ -232,46 +232,46 @@ def main():
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turb_naca0012_1c.cfg_dir = "rans_uq/naca0012"
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turb_naca0012_1c.cfg_file = "turb_NACA0012_uq_1c.cfg"
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turb_naca0012_1c.test_iter = 10
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turb_naca0012_1c.test_vals = [-4.906563, 1.338083, 6.086180, 2.412997]
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turb_naca0012_1c.test_vals = [-4.979339, 1.140084, 1.217182, 0.220079]
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test_list.append(turb_naca0012_1c)
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# NACA0012 2c
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turb_naca0012_2c = TestCase('turb_naca0012_2c')
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turb_naca0012_2c.cfg_dir = "rans_uq/naca0012"
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turb_naca0012_2c.cfg_file = "turb_NACA0012_uq_2c.cfg"
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turb_naca0012_2c.test_iter = 10
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turb_naca0012_2c.test_vals = [-5.230218, 1.262228, 6.086157, 2.412759]
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turb_naca0012_2c.test_vals = [-5.484195, 0.969780, 1.315926, 0.258346]
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test_list.append(turb_naca0012_2c)
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# NACA0012 3c
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turb_naca0012_3c = TestCase('turb_naca0012_3c')
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turb_naca0012_3c.cfg_dir = "rans_uq/naca0012"
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turb_naca0012_3c.cfg_file = "turb_NACA0012_uq_3c.cfg"
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turb_naca0012_3c.test_iter = 10
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turb_naca0012_3c.test_vals = [-5.277130, 1.246265, 6.086053, 2.412464]
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turb_naca0012_3c.test_vals = [-5.586959, 0.932347, 1.540973, 0.345562]
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test_list.append(turb_naca0012_3c)
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# NACA0012 p1c1
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turb_naca0012_p1c1 = TestCase('turb_naca0012_p1c1')
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turb_naca0012_p1c1.cfg_dir = "rans_uq/naca0012"
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turb_naca0012_p1c1.cfg_file = "turb_NACA0012_uq_p1c1.cfg"
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turb_naca0012_p1c1.test_iter = 10
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turb_naca0012_p1c1.test_vals = [-5.012946, 1.309725, 6.086066, 2.412931]
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turb_naca0012_p1c1.test_vals = [-5.132080, 1.076459, 1.183320, 0.207012]
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test_list.append(turb_naca0012_p1c1)
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# NACA0012 p1c2
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turb_naca0012_p1c2 = TestCase('turb_naca0012_p1c2')
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turb_naca0012_p1c2.cfg_dir = "rans_uq/naca0012"
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turb_naca0012_p1c2.cfg_file = "turb_NACA0012_uq_p1c2.cfg"
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turb_naca0012_p1c2.test_iter = 10
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turb_naca0012_p1c2.test_vals = [-5.264019, 1.251314, 6.086451, 2.413070]
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turb_naca0012_p1c2.test_vals = [-5.556645, 0.945121, 1.246337, 0.231311]
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test_list.append(turb_naca0012_p1c2)
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######################################
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### Harmonic Balance ###
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######################################
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######################################
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### Harmonic Balance ###
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######################################
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# Description of the regression test
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# Description of the regression test
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harmonic_balance = TestCase('harmonic_balance')
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harmonic_balance.cfg_dir = "harmonic_balance"
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harmonic_balance.cfg_file = "HB.cfg"
@@ -347,11 +347,11 @@ def main():
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ddes_flatplate.test_iter = 10
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ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783]
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ddes_flatplate.unsteady = True
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test_list.append(ddes_flatplate)
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test_list.append(ddes_flatplate)
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######################################
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### NICFD ###
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######################################
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######################################
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# Rarefaction shock wave edge_VW
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edge_VW = TestCase('edge_VW')
@@ -368,10 +368,10 @@ def main():
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edge_PPR.test_iter = 100
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edge_PPR.test_vals = [-5.401640, 0.738165, -0.000035, 0.000000]
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test_list.append(edge_PPR)
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######################################
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### Turbomachinery ###
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######################################
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######################################
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# Jones APU Turbocharger
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Jones_tc = TestCase('jones_turbocharger')
@@ -387,7 +387,7 @@ def main():
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Jones_tc_rst.cfg_dir = "turbomachinery/APU_turbocharger"
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Jones_tc_rst.cfg_file = "Jones_rst.cfg"
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Jones_tc_rst.test_iter = 5
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Jones_tc_rst.test_vals = [-4.625319, -1.569634, 34.014100, 10.187660]
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Jones_tc_rst.test_vals = [-4.626647, -1.570858, 34.014100, 10.190720]
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Jones_tc_rst.new_output = False
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test_list.append(Jones_tc_rst)
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@@ -399,7 +399,7 @@ def main():
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axial_stage2D.test_vals = [-1.933199, 5.381560, 73.357900, 1.780500]
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axial_stage2D.new_output = False
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test_list.append(axial_stage2D)
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# 2D transonic stator
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transonic_stator = TestCase('transonic_stator')
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transonic_stator.cfg_dir = "turbomachinery/transonic_stator_2D"
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transonic_stator.test_vals = [-0.563540, 5.823232, 96.736080, 0.062426]
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transonic_stator.new_output = False
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test_list.append(transonic_stator)
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# 2D transonic stator restart
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transonic_stator_rst = TestCase('transonic_stator_restart')
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transonic_stator_rst.cfg_dir = "turbomachinery/transonic_stator_2D"
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uniform_flow.test_vals = [5.000000, 0.000000, -0.188748, -10.631530]
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uniform_flow.unsteady = True
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uniform_flow.multizone = True
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test_list.append(uniform_flow)
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test_list.append(uniform_flow)
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# Channel_2D
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channel_2D = TestCase('channel_2D')
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##########################
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### FEA - FSI ###
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##########################
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##########################
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# Static beam, 3d
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statbeam3d = TestCase('statbeam3d')
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fsi2d.multizone= True
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fsi2d.unsteady = True
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test_list.append(fsi2d)
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# FSI, Static, 2D, new mesh solver
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stat_fsi = TestCase('stat_fsi')
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stat_fsi.cfg_dir = "fea_fsi/stat_fsi"
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mms_fvm_ns.test_iter = 20
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mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000]
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test_list.append(mms_fvm_ns)
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######################################
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### RUN TESTS ###
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######################################

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