n64012 Airfoil

NACA 64(1)-012 airfoil n64012 Airfoil (x,y) Coordinates 0 0 0.005 0.00978 0.0075 0.01179 0.0125 0.0149 0.025 0.02035 0.05 0.0281 0.075 0.03394 0.1 0.03871 0.15 0.0462 0.2 0.05173 0.25 0.05576 0.3…

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n6400a Airfoil

NACA 64-008A airfoil n64008a Airfoil (x,y) Coordinates 0 0 0.005 0.00646 0.0075 0.00778 0.0125 0.00983 0.025 0.01353 0.05 0.01863 0.075 0.02245 0.1 0.02559 0.15 0.03047 0.2 0.03414 0.25 0.03681 0.3…

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