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()