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Winfoil Airfoils - Total Number: 277
Name T/C % T/C Chord % Camber % Camber Chord % CL Max CD Min
NACA 663-418 17.98 44.94 2.216 50 1.394 0.0076
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NACA 4418 18 30 3.934 40 1.551 0.0104
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NACA 0219 18.99 28.73 0 0 1.427 0.013
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NACA 23021 20.95 30 1.846 10 1.121 0.0046
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NACA 654-221 20.98 39.93 1.113 50 0.646 0.0123
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