from Aerothon.ACAirfoil import ACAirfoil
import os
Michael1E423_D = ACAirfoil('Michael1E423_D', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
Michael1E423_D.PlotPolar(fig=1)
Michael1E423_D.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA2412 = ACAirfoil('NACA2412', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA2412.PlotPolar()
NACA2412.Plot2DPolar(fig=2)
NACA2412.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
Michael1 = ACAirfoil('Michael1', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
Michael1.PlotPolar()
Michael1.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
S1223RTL = ACAirfoil('S1223RTL', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
S1223RTL.PlotPolar()
S1223RTL.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
S1223THKTE = ACAirfoil('S1223THKTE', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
S1223THKTE.PlotPolar()
S1223THKTE.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
LNV109A = ACAirfoil('LNV109A', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
LNV109A.PlotPolar()
LNV109A.Plot2DPolar(fig=2)
LNV109A.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
S1223Mod = ACAirfoil('S1223Mod', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
S1223Mod.PlotPolar()
S1223Mod.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA1408 = ACAirfoil('NACA1408', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA1408.PlotPolar()
NACA1408.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA4406 = ACAirfoil('NACA4406', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA4406.PlotPolar()
NACA4406.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
Michael2 = ACAirfoil('Michael2', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
Michael2.PlotPolar()
Michael2.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
DFS03 = ACAirfoil('DFS03', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
DFS03.PlotPolar()
DFS03.Plot2DPolar(fig=2)
DFS03.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
Whale_14C = ACAirfoil('Whale_14C', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
Whale_14C.PlotPolar()
Whale_14C.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA2612 = ACAirfoil('NACA2612', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
#NACA2612.Inverted = True
NACA2612.PlotPolar()
NACA2612.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
LNV109A_9_TV = ACAirfoil('LNV109A_9_TV', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
LNV109A_9_TV.PlotPolar()
LNV109A_9_TV.Plot2DPolar(fig=2)
LNV109A_9_TV.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA4408 = ACAirfoil('NACA4408', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA4408.PlotPolar()
NACA4408.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
S1223 = ACAirfoil('S1223', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
S1223.PlotPolar()
S1223.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
LNV109A_7_12 = ACAirfoil('LNV109A_7_12', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
LNV109A_7_12.PlotPolar()
LNV109A_7_12.Plot2DPolar(fig=2)
LNV109A_7_12.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
S1223_Awesome = ACAirfoil('S1223_A', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
S1223_Awesome.PlotPolar()
S1223_Awesome.Plot2DPolar()
S1223_Awesome.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA4412 = ACAirfoil('NACA4412', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA4412.PlotPolar()
NACA4412.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
CLi4005b = ACAirfoil('CLi4005b', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
CLi4005b.PlotPolar()
CLi4005b.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA1412 = ACAirfoil('NACA1412', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA1412.PlotPolar()
NACA1412.Plot2DPolar(fig=2)
NACA1412.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA0008 = ACAirfoil('NACA0008', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
#NACA0008.Inverted = True
NACA0008.PlotPolar()
NACA0008.Plot2DPolar(fig=2)
NACA0008.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA2812 = ACAirfoil('NACA2812', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA2812.Inverted = True
NACA2812.PlotPolar()
NACA2812.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
CLi4000 = ACAirfoil('CLi4000', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
CLi4000.PlotPolar()
CLi4000.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
LNV109A_9 = ACAirfoil('LNV109A_9', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
LNV109A_9.PlotPolar()
LNV109A_9.Plot2DPolar(fig=2)
LNV109A_9.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
Baby10_S1223A_LNV109A = ACAirfoil('Baby10_S1223A_LNV109A',
fext='.txt',
nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
Baby10_S1223A_LNV109A.PlotPolar()
Baby10_S1223A_LNV109A.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA0012 = ACAirfoil('NACA0012', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA0012.PlotPolar()
NACA0012.Plot2DPolar(fig=2)
NACA0012.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
E423 = ACAirfoil('E423', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
E423.PlotPolar()
E423.PlotAirfoil(fig=2)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
E169 = ACAirfoil('E169', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
E169.PlotPolar(fig=1)
E169.Plot2DPolar(fig=2)
E169.PlotAirfoil(fig=3)
pyl.show()
from Aerothon.ACAirfoil import ACAirfoil
import os
NACA1410 = ACAirfoil('NACA1410', fext = '.txt', nalpha = 20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
NACA1410.PlotPolar()
NACA1410.PlotAirfoil(fig=2)
pyl.show()
