n63010a Airfoil

NACA 63-010A airfoil n63010a Airfoil (x,y) Co-ordinates 0 0 0.005 0.00816 0.0075 0.00983 0.0125 0.0125 0.025 0.01737 0.05 0.02412 0.075 0.02917 0.1 0.03324 0.15 0.0395 0.2 0.044 0.25 0.04714 0.3…

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