Exemplo n.º 1
0
from scalar.units import M, FT, IN, ARCDEG, RAD, LBF, SEC, KG, SLUG, OZF, gacc, GRAM, OZM
from scalar.units import AsUnit
from Aerothon.ACAircraft import ACTailAircraft
from Aerothon.ACWingWeight import ACSolidWing, ACRibWing
from Aerothon.DefaultMaterialsLibrary import Monokote, PinkFoam, Basswood, Steel, Balsa, Aluminum, Ultracote
from Fuselage_new import Fuselage
from Aircraft_Models.Reg2015Aircraft_AeroCats.Propulsion.Propulsion import Propulsion  #Reg2014-Reg2015 -Andrew Clemens
from Wing_new import Wing
import pylab as pyl
import cmath as math
from Aerothon.ACTLenAircraft import ACTLenAircraft

#
# Create the Aircraft from the ACTLenAircraft class, which limits the sum of the L,W,and H
#Length of Aircraft characteristics, Don't really need to modify this thing
Aircraft = ACTLenAircraft()
Aircraft.name = 'AeroCats_2015'  #_2014 to _2015 - Andrew Clemens
#Don't know why this is here when it is defined on line 96
Aircraft.HTailPos
# The total allowable lengths summing height + width + length of the aircraft
Aircraft.TotalLengths = 170 * IN
# Assign the already generated parts
#For Fuselage stuff go to the Fuselage script in Monowing
Aircraft.SetFuselage(Fuselage)
#Same thing with propulsion
Aircraft.SetPropulsion(Propulsion)

#
Aircraft.SetWing(Wing)

#
from scalar.units import M, FT, IN, ARCDEG, RAD, LBF, SEC, KG, SLUG, OZF, gacc, GRAM, OZM
from scalar.units import AsUnit
from Aerothon.ACAircraft import ACTailAircraft
from Aerothon.ACWingWeight import ACSolidWing, ACRibWing
from Aerothon.DefaultMaterialsLibrary import Monokote, PinkFoam, Basswood, Steel, Balsa, Aluminum, Ultracote
from Fuselage import Fuselage
from Aircraft_Models.Reg2014Aircraft_AeroCats.Propulsion.Aircraft_Propulsion import Propulsion
from Wing import Wing
import pylab as pyl
import cmath as math
from Aerothon.ACTLenAircraft import ACTLenAircraft

#
# Create the Aircraft from the ACTLenAircraft class, which limits the sum of the L,W,and H
#Length of Aircraft characteristics, Don't really need to modify this thing
Aircraft = ACTLenAircraft()
Aircraft.name = 'AeroCats_2014'
#Don't know why this is here when it is defined on line 96
Aircraft.HTailPos
# The total allowable lengths summing height + width + length of the aircraft
Aircraft.TotalLengths = 174 * IN
# Assign the already generated parts
#For Fuselage stuff go to the Fuselage script in Monowing
Aircraft.SetFuselage(Fuselage)
#Same thing with propulsion
Aircraft.SetPropulsion(Propulsion)
#
Aircraft.SetWing(Wing)

#
# Position the wing on the top of the fuselage
Exemplo n.º 3
0
from scalar.units import M, FT, IN, ARCDEG, RAD, LBF, SEC, KG, SLUG
from scalar.units import AsUnit
from Aerothon.ACAircraft import ACTailAircraft
from Aerothon.ACWingWeight import ACSolidWing, ACRibWing
from Aerothon.DefaultMaterialsLibrary import Monokote, PinkFoam, Basswood, Steel, Balsa, CarbonBar
from Fuselage import Fuselage
from Propulsion import Propulsion
from BiWing import BoxWing
import pylab as pyl
import cmath as math
from Aerothon.ACTLenAircraft import ACTLenAircraft

#
# Create the Aircraft from the ACTLenAircraft class, which limits the sum of the L,W,and H
#
Aircraft = ACTLenAircraft()
Aircraft.name = 'Aircraft2008'

#
# The total allowable lengths summing height + width + length of the aircraft
#
Aircraft.TotalLengths = 174 * IN

#
# Assign the already generated parts
#
Aircraft.SetFuselage(Fuselage)
Aircraft.SetPropulsion(Propulsion)
Aircraft.SetWing(BoxWing)

#
Exemplo n.º 4
0
from scalar.units import AsUnit
from Aerothon.ACBase import g
from Aerothon.ACAircraft import ACTailAircraft
from Aerothon.ACWingWeight import ACSolidWing, ACRibWing
from Aerothon.DefaultMaterialsLibrary import Monokote, PinkFoam, Basswood, Steel, Balsa, Aluminum
from Fuselage import Fuselage
from Aircraft_Models.Reg2009Aircraft_RedBearon.Propulsion.Propulsion import Propulsion
from BiWing import BoxWing
import pylab as pyl
import cmath as math
from Aerothon.ACTLenAircraft import ACTLenAircraft

#
# Create the Aircraft from the ACTLenAircraft class, which limits the sum of the L,W,and H
#
Aircraft = ACTLenAircraft()
Aircraft.name = 'AeroCats_2008_BoxPlane'

#
# The total allowable lengths summing height + width + length of the aircraft
#
Aircraft.TotalLengths = 174 * IN

#
# Assign the already generated parts
#
Aircraft.SetFuselage(Fuselage)
Aircraft.SetPropulsion(Propulsion)
Aircraft.SetWing(BoxWing)

#