Python TestCase.tol方法代码示例

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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"
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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 = [-2.975507,2.405636,-0.027947,0.070672 ]
    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 = [-5.868897,-5.317999,0.335382,0.022264]
    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 = [-1.810772,3.816000,-0.252360,0.044433]
    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 = [-4.722014,-4.159420,0.277228,0.018788]
    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 = [-5.236893,0.247033,-0.163494,0.013566]
    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"
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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/serial_regression/work/SU2'
    os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/serial_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 serial using autoconf
    os.system('./configure --prefix=$SU2_HOME 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)

    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 = [-2.991375,2.388702,-0.042177,0.068520]
    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 = [-5.932646,-5.394328,0.335205,0.022232]
    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 = [-1.838548,3.781222,-0.252690,0.044489]
    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_JST.cfg"
    oneram6.test_iter = 10
    oneram6.test_vals = [-4.744759,-4.182702,0.281122,0.018310]
    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 = [-5.230001,0.252184,-0.163706,0.013547]
    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 = [-6.409812,-0.945306,0.088160,-5.192708]
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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, -0.000000, 0.005688] #last 4 columns
    discadj_naca0012.su2_exec  = "SU2_CFD_AD"
    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 = [-3.724711, -4.052467, -0.000000, 0.000000] #last 4 columns
    discadj_cylinder3D.su2_exec  = "SU2_CFD_AD"
    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 = [-1.751962, 0.485775, 0.182122, -0.000018] #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 = [-1.654903, -0.491416, 0.109157, 0.000011] #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)

    #######################################
    ### 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 = [-3.391214, -2.560170, 0.000000, 0.000000] #last 4 columns
    discadj_incomp_NACA0012.su2_exec  = "SU2_CFD_AD"
    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 = [-2.802148, -2.228080, 0.000000, 0.000000] #last 4 columns
    discadj_incomp_cylinder.su2_exec  = "SU2_CFD_AD"
    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 = 10
    discadj_incomp_turb_NACA0012.test_vals = [-3.847506, -1.009607, 0.000000, 0.000000] #last 4 columns
    discadj_incomp_turb_NACA0012.su2_exec  = "SU2_CFD_AD"
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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 = [-6.145865,-5.547701,0.334821,0.022211]
    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 = [-4.825465,-4.290835,0.287910,0.015977]
    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 = [-5.232884,0.263297,0.020756,0.012889]
    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"
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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/serial_regression/work'
    os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
    os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/serial_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 serial using autoconf
    os.system('./configure --prefix=$SU2_HOME 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)

    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 = [-3.110240, 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_JST.cfg"
    oneram6.test_iter = 10
    oneram6.test_vals = [-4.704347, -4.159916, 0.271678, 0.018869] #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
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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"
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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 '=================================================================='
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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/serial_regression/work/SU2'
    os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/serial_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 serial using autoconf
    os.system('./configure --prefix=$SU2_HOME 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)

    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 = [-2.489214,2.821231,0.008730,0.053947]
    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 = [-6.203359,-5.582393,0.334818,0.022197]
    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 = [-2.703316,3.192215,-0.252410,0.044446]
    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_JST.cfg"
    oneram6.test_iter = 10
    oneram6.test_vals = [-4.830417,-4.273125,0.290066,0.015809]
    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 = [-5.227537,0.267007,-0.167233,0.012854]
    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 = [-6.764866,-1.296840,-0.024986,0.974669]
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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"
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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"
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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)

    # Fixed CL NACA0012
    fixedCL_naca0012           = TestCase('fixedcl_naca0012')
    fixedCL_naca0012.cfg_dir   = "fixed_cl/naca0012"
    fixedCL_naca0012.cfg_file  = "inv_NACA0012.cfg"
    fixedCL_naca0012.test_iter = 500
    fixedCL_naca0012.test_vals = [-5.930145,-0.546310,0.300089,0.019393] #last 4 columns
    fixedCL_naca0012.su2_exec  = "parallel_computation.py -f"
    fixedCL_naca0012.timeout   = 1600
    fixedCL_naca0012.tol       = 0.00001
    test_list.append(fixedCL_naca0012)
    
    # Polar sweep of the inviscid NACA0012
    polar_naca0012           = TestCase('polar_naca0012')
    polar_naca0012.cfg_dir   = "polar/naca0012"
    polar_naca0012.cfg_file  = "inv_NACA0012.cfg"
    polar_naca0012.polar     = True
    polar_naca0012.test_iter = 10
    polar_naca0012.test_vals = [-1.298373, 4.139860, 0.010703, 0.008932] #last 4 columns
    polar_naca0012.su2_exec  = "compute_polar.py -i 11"
    polar_naca0012.timeout   = 1600
    polar_naca0012.tol       = 0.00001
    test_list.append(polar_naca0012)

    ##########################
    ###  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
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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, -0.000000, 0.005688] #last 4 columns
    discadj_naca0012.su2_exec  = "SU2_CFD_AD"
    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 = [-3.724711, -4.052467, -0.000000, 0.000000] #last 4 columns
    discadj_cylinder3D.su2_exec  = "SU2_CFD_AD"
    discadj_cylinder3D.timeout   = 1600
    discadj_cylinder3D.tol       = 0.00001
    test_list.append(discadj_cylinder3D)

    # Arina nozzle 2D  
    discadj_arina2k              = TestCase('discadj_arina2k')
    discadj_arina2k.cfg_dir      = "disc_adj_euler/arina2k"
    discadj_arina2k.cfg_file     = "Arina2KRS.cfg"
    discadj_arina2k.test_iter    = 20
    discadj_arina2k.test_vals    = [-0.774805, -0.801209, 3.1979e+02, 0.0000e+00] #last 4 columns
    discadj_arina2k.su2_exec     = "SU2_CFD_AD"
    discadj_arina2k.timeout      = 8400
    discadj_arina2k.tol          = 0.00001
    test_list.append(discadj_arina2k)

    #######################################################
    ### 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 = [-1.751962, 0.485751, 0.182121, -0.000018] #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 = [-1.654903, -0.491485, 0.109157, 0.000011] #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)

    #######################################
    ### Disc. adj. incompressible Euler ###
    #######################################

    # Adjoint Incompressible Inviscid NACA0012
    discadj_incomp_NACA0012           = TestCase('discadj_incomp_NACA0012')
    discadj_incomp_NACA0012.cfg_dir   = "disc_adj_incomp_euler/naca0012"
    discadj_incomp_NACA0012.cfg_file  = "incomp_NACA0012_disc.cfg"
    discadj_incomp_NACA0012.test_iter = 20
    discadj_incomp_NACA0012.test_vals = [-3.633197, -2.544956, 0.000000, 0.000000] #last 4 columns
    discadj_incomp_NACA0012.su2_exec  = "SU2_CFD_AD"
    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 (Heated)
    discadj_incomp_cylinder           = TestCase('discadj_incomp_cylinder')
    discadj_incomp_cylinder.cfg_dir   = "disc_adj_incomp_navierstokes/cylinder"
    discadj_incomp_cylinder.cfg_file  = "heated_cylinder.cfg"
    discadj_incomp_cylinder.test_iter = 20
    discadj_incomp_cylinder.test_vals = [-2.374306, -2.371564, 0.000000, 0.000000] #last 4 columns
    discadj_incomp_cylinder.su2_exec  = "SU2_CFD_AD"
    discadj_incomp_cylinder.timeout   = 1600
    discadj_incomp_cylinder.tol       = 0.00001
    test_list.append(discadj_incomp_cylinder)

#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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"
#.........这里部分代码省略.........

# 需要导入模块: from TestCase import TestCase [as 别名]
# 或者: from TestCase.TestCase import tol [as 别名]
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"
#.........这里部分代码省略.........