def setup(self, N=5):
exec parse_variables(Wing.__doc__)
self.wing = WingGP.setup(self, N=N)
with SignomialsEnabled():
constraints = [mw * (1 + 2 / self.planform["AR"]) >= 2 * np.pi]
return self.wing, constraints
def setup(self, N=5):
self.wing = WingGP.setup(self, N=N)
mw = Variable("m_w", "-", "span wise effectiveness")
with SignomialsEnabled():
constraints = [mw * (1 + 2 / self.planform["AR"]) >= 2 * np.pi]
return self.wing, constraints
def setup(self, N=3):
exec parse_variables(VerticalTail.__doc__)
self.ascs = Wing.setup(self, N)
self.planform.substitutions.update(
{self.planform.tau: 0.08, self.planform.lam: 0.8,
self.planform.AR: 4})
if self.fillModel:
self.foam.substitutions.update({self.foam.Abar: 0.0548,
self.foam.material.rho: 0.024})
return self.ascs
def setup(self, N=3):
exec parse_variables(HorizontalTail.__doc__)
self.ascs = Wing.setup(self, N)
self.planform.substitutions.update({
self.planform.AR: 4,
self.planform.lam: 0.8
})
if self.fillModel:
self.foam.substitutions.update({
self.foam.Abar: 0.0548,
self.foam.material.rho: 0.024
})
return self.ascs, mh * (1 + 2.0 / self.planform["AR"]) <= 2 * np.pi