#==============================================================================#
# AIRCRAFT MODEL
#==============================================================================#
# Create the Aircraft from the ACTailAircraft class imported above from Aerothon
Aircraft = ACTailAircraft()
#Aircraft = ACTLenAircraft()
Aircraft.name = 'Regular 2019: The Fellowship of the Wing'
# Assign parts we imported above (generated outside of this script) to aircraft
Aircraft.SetWing(Wing)
Aircraft.SetFuselage(Fuselage)
Aircraft.SetPropulsion(Propulsion)
# Wing alignment
Aircraft.WingFuseFrac = 0 # 0.0 @ bottom of fuselage; 1.0 @ top of fuselage
Aircraft.Wing.i = 0 * ARCDEG # induced angle of attack, wing incidence
#Aircraft.Wing.X[0] = 20*IN
# Engine alignment (height)
Aircraft.EngineAlign = 0.72 #this doesnt seem to be doing anything
# Aircraft Properties
EmptyWeight = 17 * LBF # dechellis: estimated airframe weight
TennisBalls = 60.0 # dechellis: number of tennis balls flying
BallWeight = 0.131333 * LBF # dechellis: weight of 1 tennis ball
PayloadWeight = (0.50 * LBF +
BallWeight) * TennisBalls # dechellis: "passenger luggage"
Fuselage.PayBay.TennisBalls.Weight = BallWeight * TennisBalls # Reassign tennis ball weight distribution based off desired loading
Aircraft.TotalWeight = PayloadWeight + EmptyWeight # needed for calculations
Aircraft.TippingAngle = 10 * ARCDEG # Black line on AC plot, set to Lift Off AoA
from Adv2020Aircraft.Aircraft_Core_Design.Propulsion import Propulsion from Adv2020Aircraft.Aircraft_Core_Design.Wing import Wing import pylab as pyl # # Create the Aircraft from the ACTailAircraft class Aircraft = ACTailAircraft() Aircraft.name = 'AdvAeroCats_2020' # # Assign the already generated parts Aircraft.SetFuselage(Fuselage) Aircraft.SetPropulsion(Propulsion) Aircraft.SetWing(Wing) # # Position the wing on the top of the fuselage Aircraft.WingFuseFrac = 0.3 Aircraft.Wing.i = 0 * ARCDEG # # Aircraft Properties # Total weight is going to change Aircraft.TotalWeight = 54 * LBF # Engine align Aircraft.EngineAlign = 0 Aircraft.TippingAngle = 15 * ARCDEG # Black line on AC plot Aircraft.RotationAngle = 12 * ARCDEG # Red line on AC plot Aircraft.Alpha_Groundroll = 0 * ARCDEG Aircraft.CMSlopeAt = (0 * ARCDEG, 10 * ARCDEG) Aircraft.CLSlopeAt = (0 * ARCDEG, 15 * ARCDEG) Aircraft.CLHTSlopeAt = (0 * ARCDEG, 15 * ARCDEG)
# Create the Aircraft from the ACTailAircraft class #`` Aircraft = ACTailAircraft() Aircraft.name = 'AdvAeroCats_2014' # # Assign the already generated parts # Aircraft.SetFuselage(Fuselage) Aircraft.SetPropulsion(Propulsion) Aircraft.SetWing(Wing) # # Position the wing on the top of the fuselage # Aircraft.WingFuseFrac = 1.05 Aircraft.Wing.i = 0 * ARCDEG # # Aircraft Properties # Total weight is going to change Aircraft.TotalWeight = 27 * LBF # Engine align Aircraft.EngineAlign = 1.0 Aircraft.TippingAngle = 8.5 * ARCDEG # Black line on AC plot, set to Lift Off AoA Aircraft.RotationAngle = 15 * ARCDEG # Red line on AC plot, set 15 deg Aircraft.Alpha_Groundroll = 0 * ARCDEG Aircraft.CMSlopeAt = (2 * ARCDEG, 10 * ARCDEG) Aircraft.CLSlopeAt = (3 * ARCDEG, 14 * ARCDEG) Aircraft.CLHTSlopeAt = (-5 * ARCDEG, 10 * ARCDEG)