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Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
NACA 2418 17.96 30 1.95 40 1.367 0.0128
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NACA 653-218 17.97 39.94 1.118 50 1.172 0.0034
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NACA 653-418 17.97 39.88 2.221 50 1.41 0.0082
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NACA 653-618 17.97 39.826 3.324 50 1.618 0.0085
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NACA 663-218 17.97 44.97 1.117 50 1.166 0.0073
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