def Rendering(obj):
display, start_display, add_menu, add_function_to_menu = init_display()
# Printing the variables from the aircraft object...
# attrs = vars(aircraft)
# pprint.pprint(attrs,width=1)
#------------- WING --------------------
# Add NACA 4 digit airfoils to loft between:
x0 = float(obj.geo['Kink_wing']['x'][0])
y0 = float(obj.geo['Kink_wing']['y'][0])
z0 = 0.0
c0 = float(obj.geo['Kink_wing']['chords'][0])
# z0 = obj.geo['Kink_wing']['zu'][0]
x1 = float(obj.geo['Kink_wing']['x'][1])
y1 = float(obj.geo['Kink_wing']['y'][1])
z1 = 0.0
c1 = float(obj.geo['Kink_wing']['chords'][1])
#
x2 = float(obj.geo['Kink_wing']['x'][2])
y2 = float(obj.geo['Kink_wing']['y'][2])
z2 = 0.0
c2 = float(obj.geo['Kink_wing']['chords'][2])
#
x3 = float(obj.geo['Kink_wing']['x'][3])
y3 = float(obj.geo['Kink_wing']['y'][3])
z3 = 0.0
c3 = float(obj.geo['Kink_wing']['chords'][3])
# Profiles...
Af0 = airconics.primitives.Airfoil([x0, y0, z0],
ChordLength=c0,
Rotation=0,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af0.Curve, update=True, color='GREEN')
Af1 = airconics.primitives.Airfoil([x1, y1, z1],
ChordLength=c1,
Rotation=0,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af1.Curve, update=True, color='GREEN')
Af2 = airconics.primitives.Airfoil([x2, y2, z2],
ChordLength=c2,
Rotation=0,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af2.Curve, update=True, color='GREEN')
Af3 = airconics.primitives.Airfoil([x3, y3, z3],
ChordLength=c3,
Rotation=0,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af3.Curve, update=True, color='GREEN')
surf_wingin = act.AddSurfaceLoft([Af0, Af1, Af2])
surf_wingout = act.AddSurfaceLoft([Af2, Af3])
#------------- HT --------------------
# Add NACA 4 digit airfoils to loft between:
x0 = float(obj.geo['horz']['x'][0])
y0 = float(obj.geo['horz']['y'][0])
z0 = 0.0
c0 = float(obj.geo['horz']['chords'][0])
# z0 = obj.geo['Kink_wing']['zu'][0]
x1 = float(obj.geo['horz']['x'][1])
y1 = float(obj.geo['horz']['y'][1])
z1 = 0.0
c1 = float(obj.geo['horz']['chords'][1])
x2 = float(obj.geo['horz']['x'][2])
y2 = float(obj.geo['horz']['y'][2])
z2 = 0.0
c2 = float(obj.geo['horz']['chords'][2])
# Profiles...
Af0 = airconics.primitives.Airfoil([x0, y0, z0],
ChordLength=c0,
Rotation=0,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af0.Curve, update=True, color='GREEN')
Af1 = airconics.primitives.Airfoil([x1, y1, z1],
ChordLength=c1,
Rotation=0,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af1.Curve, update=True, color='GREEN')
Af2 = airconics.primitives.Airfoil([x2, y2, z2],
ChordLength=c2,
Rotation=0,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af2.Curve, update=True, color='GREEN')
surf_HT = act.AddSurfaceLoft([Af0, Af1, Af2])
#------------- VT --------------------
# Add NACA 4 digit airfoils to loft between:
# x0 = float(obj.geo['vert']['x'][0])
# y0 = 0.0
# z0 = float(obj.geo['vert']['z'][0])
x0 = float(obj.geo['vert']['x'][0])
y0 = 0.0
z0 = 1.0
c0 = float(obj.geo['vert']['chords'][0])
# z0 = obj.geo['Kink_wing']['zu'][0]
#x1 = float(obj.geo['vert']['x'][1])
#y1 = 0.0
# z1 = float(obj.geo['vert']['z'][0])
x1 = float(obj.geo['vert']['x'][1])
y0 = 0.0
z1 = 5.5
c1 = float(obj.geo['vert']['chords'][1])
# Profiles...
Af0 = airconics.primitives.Airfoil([x0, y0, z0],
ChordLength=c0,
Rotation=90,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af0.Curve, update=True, color='GREEN')
Af1 = airconics.primitives.Airfoil([x1, y1, z1],
ChordLength=c1,
Rotation=90,
Twist=0,
Naca4Profile='0012')
display.DisplayShape(Af1.Curve, update=True, color='GREEN')
surf_VT = act.AddSurfaceLoft([Af0, Af1])
#------------- FUSELAGE --------------------
##
# fus = fuselage_oml.Fuselage(NoseLengthRatio=0.182,
# TailLengthRatio=0.293,
# Scaling=[55.902, 55.902, 55.902],
# NoseCoordinates=[0.0, 0.0, 0],
# CylindricalMidSection=False,
# SimplificationReqd=False,
# Maxi_attempt=5,
# construct_geometry=True)
# Current Display of the WHTVT
display.DisplayShape(surf_wingin, update=True)
display.DisplayShape(surf_wingout, update=True)
display.DisplayShape(surf_HT, update=True)
display.DisplayShape(surf_VT, update=True)
#display.DisplayShape(fus, update=True)
# fus.Display()
start_display()
"""
if __name__ == "__main__":
import airconics
import airconics.AirCONICStools as act
# Initialise the display
from OCC.Display.SimpleGui import init_display
display, start_display, add_menu, add_function_to_menu = init_display()
# Add NACA 4 digit airfoils to loft between:
Af2 = airconics.primitives.Airfoil([0., 0., 0.],
ChordLength=3.,
Naca4Profile='2412')
display.DisplayShape(Af2.Curve, update=True, color='GREEN')
Af3 = airconics.primitives.Airfoil([0., 5., 0.],
ChordLength=1.,
Naca4Profile='0012')
display.DisplayShape(Af3.Curve, update=True, color='GREEN')
Af4 = airconics.primitives.Airfoil([0., 6., 0.2],
ChordLength=0.2,
Naca4Profile='0012')
display.DisplayShape(Af4.Curve, update=True, color='GREEN')
surf = act.AddSurfaceLoft([Af2, Af3, Af4])
# Note that surf is a TOPO_DS Shape, and hence no surf.Shape is required for display
display.DisplayShape(surf, update=True)
start_display()