def __init__(self, T3t=k.T3t, T0=k.T0, Pa=k.Pa, delta=0.01, verbose=True):
self.delta = delta
self.data = Problem1.empty_data_array(delta)
self.T3t = T3t
self.T0 = T0
self.Pa = Pa
self.verbose = verbose
self.P2 = Problem2()
def __init__(self, T3t=k.T3t, T0=k.T0, Pa=k.Pa, delta=0.01, gamma=k.GAMMA, verbose=True):
self.delta = delta
self.data = Problem1.empty_data_array(delta)
self.P1 = Problem1(verbose=False)
self.SF_P1, self.M0_P1 = self.P1.SF, self.P1.M0
self.M0, self.SF = 0, 0
self.air = pm.get('ig.air')
self.T3t = T3t
self.T0 = T0
self.Pa = Pa
self.M4 = 2
self.gamma = gamma
self.verbose = verbose
self.ideal_nozzle()
def __init__(self,
T3t=k.T3t,
T0=k.T0,
Pa=k.Pa,
delta=0.01,
gamma=k.GAMMA,
verbose=True):
self.delta = delta
self.data = Problem1.empty_data_array(delta)
self.P1 = Problem1(verbose=False)
self.SF_P1, self.M0_P1 = self.P1.SF, self.P1.M0
self.air = pm.get('ig.air')
self.T3t = T3t
self.T0 = T0
self.Pa = Pa
self.gamma = gamma
self.verbose = verbose
self.M0_star = self.equation_A()
#self.optimize()
self.M4 = 2.53
self.A = self.equation_B(self.M4)
#self.nozzle_area_ratio = self.equation_B()
self.execute()