Exemplo n.º 1
0
from __future__ import division  # let 5/2 = 2.5 rather than 2
#from os import environ as _environ; _environ["scalar_off"] = "off"

from Aircraft_Models.Adv2014Aircraft_AeroCats.MonoWing.Aircraft import Aircraft
import pylab as pyl

Aircraft.PlotTailLoad(fig=2)
Aircraft.Draw()
pyl.show()
Exemplo n.º 2
0
#from Aircraft_158 import Aircraft
#from Aircraft_160 import Aircraft

#from Aircraft_Models.Reg2013Aircraft_AeroCats.MonoWing.AircraftGE import Aircraft
#from Aircraft_144GE import Aircraft
#from Aircraft_148GE import Aircraft
#from Aircraft_150GE import Aircraft
#from Aircraft_152GE import Aircraft
#from Aircraft_154GE import Aircraft
#from Aircraft_155GE import Aircraft
#from Aircraft_156GE import Aircraft
#from Aircraft_158GE import Aircraft

#from Aircraft_Models.Reg2013Aircraft_AeroCats.TradeStudies.LowMoment.Aircraft import Aircraft

Aircraft.Draw(fig=2)
pyl.figure(1)

#
# Get the design point
#
dsgnGR = Aircraft.Groundroll() / (FT)
dsgnCR = Aircraft.Rate_of_Climb() / (FT / MIN)
pyl.plot([dsgnCR], [dsgnGR], 'ro', markersize=8)

#
# Set up ranges
#
S = npy.linspace(1800, 3200, 4) * IN**2
TotalWeight = npy.linspace(27, 30, 5) * LBF