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
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
E169_101 = ACAirfoil('E169_101', fext='.txt', nalpha=20)
if __name__ == '__main__':
import pylab as pyl
#
# Plot the polars and the airfoil
#
#E169_101.PlotPolar(fig=1)
E169_101.Plot2DPolar(fig=2)
#E169_101.PlotAirfoil(fig=3)
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
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
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
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
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
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
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
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
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()
