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Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
NACA 6409 9.04 50 5.973 40 1.383 0
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NACA 6412 12.06 50 5.981 40 1.535 0.0075
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NACA 64A210 9.97 39.96 1.325 49.99 0.558 0.0004
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NACA 64A-312 11.95 38.26 1.554 51.68 1.059 0.009
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NACA 64A410 9.96 38.26 2.115 51.68 1.065 0.0009
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