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()