本文整理匯總了Python中TestCase.TestCase類的典型用法代碼示例。如果您正苦於以下問題：Python TestCase類的具體用法？Python TestCase怎麽用？Python TestCase使用的例子？那麽, 這裏精選的類代碼示例或許可以為您提供幫助。
在下文中一共展示了TestCase類的15個代碼示例，這些例子默認根據受歡迎程度排序。您可以為喜歡或者感覺有用的代碼點讚，您的評價將有助於係統推薦出更棒的Python代碼示例。
示例1: runBenchmark
def runBenchmark(self,benchmark,stdout):
config = self.getConfiguration()
testCase = TestCase(config,stdout)
testCase.prepare(benchmark)
self.scanFedSizes(benchmark,testCase)
testCase.destroy()示例2: run
def run(self, stdout):
logging.info("RestartableRunner.run() called")
self.testRunner.startLaunchers()
# TODO: check if all launchers are responding (with timeout)
# instead of waiting for a fixed amount of time
time.sleep(5)
configData = self.testRunner.getAllConfigurations()[0]
config = configData['config']
testName = configData['name']
try:
while not self.stopFlag:
try:
self.testCase = TestCase(config, stdout, afterStartupCallback=self.afterStartupCallback)
self.testCase.prepare(testName)
fragSize = self.testRunner.getFedSizes()
assert len(fragSize) == 1
fragSize = fragSize[0]
fragSizeRMS = int(fragSize * self.testRunner.args['rms'])
# this should only terminate when the user terminates the optimization
self.testCase.runScan(fragSize, fragSizeRMS, self.testRunner.args)
# evb was stopped
self.evbStarted.clear()
self.evbStopped.set()
self.testCase.destroy()
self.testCase = None
except BadConfig:
self.stopFlag = True
sys.exit(1)
finally:
self.testRunner.stopLaunchers()示例3: TestCaseTest
class TestCaseTest(TestCase):
def setUp(self):
self.result = TestResult()
def testTemplateMethod(self):
test = WasRun("testMethod")
test.run(self.result)
assert "setUp testMethod tearDown" == test.log
def testResult(self):
test = WasRun("testMethod")
test.run(self.result)
assert "1 run, 0 failed" == self.result.summary()
def testFailedResultFormatting(self):
self.result.testStarted()
self.result.testFailed()
assert "1 run, 1 failed" == self.result.summary()
def testFailedResult(self):
self.test = WasRun("testBrokenMethod")
self.test.run(self.result)
assert "1 run, 1 failed" == self.result.summary()
def checkForLog(self):
self.test = WasRun("testMethod")
self.test.run(self.result)
assert path.isfile("C:/Nathans Python Folder/log.txt")
def testSetUpException(self):
self.test = TestCase("setUp")
self.test.run(self.result)
assert "1 run, 1 failed" == self.result.summary()
def testSuite(self):
suite = TestSuite()
suite.add(TestCaseTest("testFailedResultFormatting"))
suite.add(TestCaseTest("setUp"))
suite.add(TestCaseTest("testTemplateMethod"))
suite.add(WasRun("testMethod"))
suite.add(TestCaseTest("testResult"))
suite.add(WasRun("testBrokenMethod"))
suite.add(TestCaseTest("testSetUpException"))
suite.run(self.result)
assert "6 run, 2 failed" == self.result.summary()示例4: testThatEvenMoreFilesAreExcluded
def testThatEvenMoreFilesAreExcluded(self):
expectedOutput = \
self.getBaseDir() + """CgrepTest/a.html:1:needle
"""
self._CfgrepTest1("needle", "needle", expectedOutput)
def _CfgrepTest1(self, actualNeedle, searchNeedle, expectedOutput, extraParameters=""):
os.system("rm -rf CgrepTest")
os.mkdir("CgrepTest")
os.system("echo %s > CgrepTest/a.html"% actualNeedle) # Will list this file
os.mkdir("CgrepTest/vehicles")
os.system("echo %s > CgrepTest/vehicles/a"% actualNeedle)
os.mkdir("CgrepTest/states")
os.system("echo %s > CgrepTest/states/a"% actualNeedle)
os.mkdir("CgrepTest/states2")
os.system("echo %s > CgrepTest/states2/a"% actualNeedle)
command = "~/svn/devscripts/bin/%s %s %s %s"% (self.getCommand(), searchNeedle, self.myTestDir, extraParameters)
procHandle = os.popen(command)
output = procHandle.read()
os.system("rm -rf CgrepTest")
self.myAssertEqual(expectedOutput, output)
def getCommand(self):
return "cfgrep"
if __name__ == "__main__":
TestCase.main()
示例5: main
def main():
"""This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. """
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase("channel")
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.071007, 2.301191, 0.008562, 0.028922] # last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase("naca0012")
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] # last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase("wedge")
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.690232, 3.924432, -0.252221, 0.044419] # last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase("oneram6")
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.400678, -12.932056, 0.282557, 0.012706] # last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase("flatplate")
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231727, 0.261637, -0.166869, 0.012707] # last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase("cylinder")
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] # last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase("cylinder_lowmach")
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.861860, -1.399846, -1.557250, 110.230719] # last 4 columns
cylinder_lowmach.su2_exec = "parallel_computation.py -f"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase("rae2822_sa")
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
#.........這裏部分代碼省略.........
示例6: main
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606841, -9.035214, -0.000000, 0.005688] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.720476, -4.039256, 0.000000, 0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "parallel_computation.py -f"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751965, 0.485796, 0.182895, -0.000018] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.654193, -0.499281, 0.145545, -0.000018] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [-2.917789, -2.714752, 0.000000, 0.000000] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder_disc.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [-2.727423, -2.272530, 0.000000, 0.000000] #last 4 columns
discadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012
discadj_incomp_turb_NACA0012 = TestCase('discadj_incomp_turb_NACA0012')
discadj_incomp_turb_NACA0012.cfg_dir = "incomp_rans/naca0012"
discadj_incomp_turb_NACA0012.cfg_file = "naca0012_disc.cfg"
discadj_incomp_turb_NACA0012.test_iter = 100
discadj_incomp_turb_NACA0012.test_vals = [-3.645810, -1.625922, 0.000000, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012.su2_exec = "parallel_computation.py -f"
#.........這裏部分代碼省略.........
示例7: __init__
def __init__(self, name):
TestCase.__init__(self, name)示例8: main
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['TEST_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work'
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync Test Cases repo
os.chdir( os.environ['TEST_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --enable-mpi --with-cc=`which mpicc` --with-cxx=`which mpicxx` CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.984481, 2.389875, 0.008865, 0.027854] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.702502, 3.923373, -0.252116, 0.044396] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.701280, -4.154921, 0.270257, 0.019095] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.233923, 0.259801, -0.166790, 0.012722] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
#.........這裏部分代碼省略.........
示例9: main
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606839,-9.035212,-3.3386e-07,1.8777e-01] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751947, 0.485758, 0.181440, -0.385110] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.658566, -0.487694, 0.087556, -0.537010] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 10
discadj_cylinder.test_vals = [3.522068,-1.787841,-1.2030e-02,1.1156e-03] #last 4 columns
discadj_cylinder.su2_exec = "SU2_CFD_AD"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN PYTHON TESTS ###
######################################
# test discrete_adjoint.py
discadj_euler_py = TestCase('discadj_euler_py')
discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
discadj_euler_py.cfg_file = "inv_NACA0012.cfg"
discadj_euler_py.test_iter = 10
discadj_euler_py.su2_exec = "discrete_adjoint.py"
discadj_euler_py.timeout = 1600
discadj_euler_py.reference_file = "of_grad_cd_disc.dat.ref"
discadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_euler_py.run_filediff())
test_list.append(discadj_euler_py)
# test direct_differentiation.py
directdiff_euler_py = TestCase('directdiff_euler_py')
directdiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
directdiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
directdiff_euler_py.test_iter = 10
directdiff_euler_py.su2_exec = "direct_differentiation.py"
directdiff_euler_py.timeout = 1600
directdiff_euler_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_euler_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_euler_py.run_filediff())
test_list.append(directdiff_euler_py)
# Tests summary
print '=================================================================='
#.........這裏部分代碼省略.........
示例10: main
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686, 0.029098] #last 4 columns
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.191618, -5.592802, 0.334809, 0.022197] #last 4 columns
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.711318, 3.913749, -0.252131, 0.044402] #last 4 columns
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.393130, -12.928941, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231916, 0.261866, -0.166832, 0.012717] #last 4 columns
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019496, 0.310082] #last 4 columns
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442524, -5.441383, 0.884279, 0.024730] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
#.........這裏部分代碼省略.........
示例11: main
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --with-MPI=mpicxx CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.007706, 2.358555, 0.008379, 0.028547]
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.157022, -5.537399, 0.334831, 0.022209]
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.647184, 3.989725, -0.251604, 0.044317]
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.707461, -4.138449, 0.269324, 0.018891]
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.232930, 0.260877, -0.166066, 0.013093]
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
#.........這裏部分代碼省略.........
示例12: main
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git pull')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --with-MPI=mpicxx CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.413846,2.965840,0.007590,0.051651]
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-3.751809,-3.271265,0.136604,0.066791]
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-2.694577,3.148295,-0.252137,0.044398]
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.819412,-4.286432,0.288842,0.016334]
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.142353,0.347570,0.029870,0.015971]
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
#.........這裏部分代碼省略.........
示例13: main
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.071007, 2.301191, 0.008562, 0.028922] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.690232, 3.924432, -0.252221, 0.044419] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.400678, -12.932056, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231743, 0.261628, -0.166871, 0.012706] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.861860, -1.399846, -1.557250, 110.230719] #last 4 columns
cylinder_lowmach.su2_exec = "parallel_computation.py -f"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
#.........這裏部分代碼省略.........
示例14: testSetUpException
def testSetUpException(self):
self.test = TestCase("setUp")
self.test.run(self.result)
assert "1 run, 1 failed" == self.result.summary()示例15: __init__
def __init__(self, name):
self.wasRun = None
TestCase.__init__(self, name)