def make_Wing(wing_Side='Right'):
# Prep the airfoil blank
airfoil_Blank = Polygon(points=config.Airfoil.airfoil_Points)
# Resize airfoil chord to target chord.
airfoil_Blank.scale(config.Airfoil.aerofoil_Calculated_Chord,
config.Airfoil.aerofoil_Calculated_Chord, 1)
# Make the airfoil
airfoil = utilities.extrude_Blank(airfoil_Blank)
# Cut the aileron holes
diff_Aileron(airfoil)
# Tilt and mirror the wing
if (wing_Side == 'Right'):
# Tilt the airfoil
rotation_Angle = (-1) * config.Wing.wing_Bend_Angle
airfoil.rotate(0, rotation_Angle, 0)
else:
# Rotate the airfoil in the opposide direction
rotation_Angle = (-1) * config.Wing.wing_Bend_Angle
airfoil.rotate(0, rotation_Angle, 0)
# Mirror the airfoil
airfoil.mirror([1, 0, 0])
return airfoil
def make_Wing(wing_Side = 'Right'):
# Prep the airfoil blank
airfoil_Blank = Polygon(points=config.Airfoil.airfoil_Points)
# Resize airfoil chord to target chord.
airfoil_Blank.scale(config.Airfoil.aerofoil_Calculated_Chord, config.Airfoil.aerofoil_Calculated_Chord, 1)
# Make the airfoil
airfoil = utilities.extrude_Blank(airfoil_Blank)
# Cut the aileron holes
diff_Aileron(airfoil)
# Tilt and mirror the wing
if (wing_Side == 'Right'):
# Tilt the airfoil
rotation_Angle = (-1) * config.Wing.wing_Bend_Angle
airfoil.rotate(0, rotation_Angle, 0)
else:
# Rotate the airfoil in the opposide direction
rotation_Angle = (-1) * config.Wing.wing_Bend_Angle
airfoil.rotate(0, rotation_Angle, 0)
# Mirror the airfoil
airfoil.mirror([1,0,0])
return airfoil
def diff_Aileron(airfoil):
# Make the cutting blank
# Make a square.
blank = Polygon(points=config.Aileron.aileron_Blank_Points)
# Rotate it so that it is parallel to the direction of the aircraft
blank.rotate(90,90,0)
# Scale it to the appropriate size
# Maths:
# For ever mm of chord, the max thickness of the wing is 0.1mm.
# Therefore, the aileron thickness should be at least 0.2 times the chord, and the length can be however long we want.
#blank.scale()
# Extrude the blank so that we can use it as a differencing object
blank = utilities.extrude_Blank(blank, extrusion_Bounds = config.Aileron.aileron_Bounds)
return airfoil
def diff_Aileron(airfoil):
# Make the cutting blank
# Make a square.
blank = Polygon(points=config.Aileron.aileron_Blank_Points)
# Rotate it so that it is parallel to the direction of the aircraft
blank.rotate(90, 90, 0)
# Scale it to the appropriate size
# Maths:
# For ever mm of chord, the max thickness of the wing is 0.1mm.
# Therefore, the aileron thickness should be at least 0.2 times the chord, and the length can be however long we want.
#blank.scale()
# Extrude the blank so that we can use it as a differencing object
blank = utilities.extrude_Blank(
blank, extrusion_Bounds=config.Aileron.aileron_Bounds)
return airfoil
