def __init__(self, T=None, U=None, p=None, k=None, epsilon=None, nut=None):
"""Init bounday condition."""
# set default values for an inlet
U = U or InletOutlet('uniform (0 0 0)', '$internalField')
p = p or FixedValue('$pressure')
k = k or InletOutlet('uniform $turbulentKE', '$internalField')
epsilon = epsilon or InletOutlet('uniform $turbulentEpsilon',
'$internalField')
nut = nut or Calculated('0')
T = T or ZeroGradient()
super(WindTunnelOutletBoundaryCondition,
self).__init__('patch', T, U, p, k, epsilon, nut)
def __init__(self, T=None, U=None, p=None, k=None, epsilon=None, nut=None,
alphat=None, p_rgh=None):
"""Init bounday condition."""
# set default values for an inlet
U = U or InletOutlet(value='uniform (0 0 0)', inletValue='uniform (0 0 0)')
p = p or FixedValue('0')
k = k or InletOutlet(value='uniform 0.1', inletValue='uniform 0.1')
epsilon = epsilon or InletOutlet(value='uniform 0.1', inletValue='uniform 0.1')
nut = Calculated('0')
T = T or ZeroGradient()
alphat = alphat or ZeroGradient()
p_rgh = p_rgh or FixedValue('0')
super(FixedOutletBoundaryCondition, self).__init__(
'patch', T, U, p, k, epsilon, nut, alphat, p_rgh
)