from Aerothon.ACAirfoil import ACAirfoil
import pylab as pyl
afv = ACAirfoil('/NACA0012/NACA0012.dat','NACA0012')
afh = ACAirfoil('clarky/clarky.dat','clarky')
afh.Inverted = True
afv.PlotAirfoil(1)
afh.PlotAirfoil(2)
pyl.figure(1)
pyl.title('Vertical Tail Airfoil')
pyl.grid()
pyl.figure(2)
pyl.title('Horizontal Tail Airfoil')
pyl.grid()
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()
