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Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
NACA 63-206 5.99 34.97 1.108 50 0.62 0.0052
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NACA 63-209 8.99 34.96 1.11 50 0.756 0.006
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NACA 63-210 9.98 34.95 1.11 50 0.961 0.0061
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NACA 632-215 14.97 34.93 1.114 50 0.998 0.0052
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NACA 632-415 14.98 34.85 2.213 50 1.268 0.0028
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