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Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
NACA 4510 8.01 28.39 6.438 46.85 0.741 0.0145
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NACA 4512 12.2 26.89 3.257 51.63 1.25 0.0059
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NACA 63-010 9.98 35 0 0 0.699 0.0065
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NACA 631-212 11.98 34.94 1.108 50 1.071 0.0068
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NACA 631-412 11.98 34.88 2.215 50 1.268 0.007
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