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()