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prop_test.py
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prop_test.py
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" propeller tests "
from gpkitmodels.GP.aircraft.prop.propeller import Propeller, ActuatorProp
from gpkitmodels.GP.aircraft.prop.propeller import MultiElementProp
from gpkitmodels.GP.aircraft.wing.wing_test import FlightState
from gpkit import units, Model
def simpleprop_test():
" test simple propeller model "
fs = FlightState()
Propeller.flight_model = ActuatorProp
p = Propeller()
pp = p.flight_model(p, fs)
m = Model(1/pp.eta + p.W/(100.*units("lbf"))+ pp.Q/(100.*units("N*m")),
[fs, p, pp])
m.substitutions.update({"rho": 1.225, "V": 50, "T": 100, "omega":1000})
sol = m.solve()
def ME_eta_test():
fs = FlightState()
Propeller.flight_model = MultiElementProp
p = Propeller()
pp = p.flight_model(p,fs)
pp.substitutions[pp.T] = 100
pp.cost = 1./pp.eta + pp.Q/(100.*units("N*m")) + p.T_m/(1000*units('N'))
sol = pp.localsolve(iteration_limit = 400)
def test():
"tests"
simpleprop_test()
ME_eta_test()
if __name__ == "__main__":
test()