Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
---|---|---|---|---|---|---|---|
NACA 66-209 | 8.98 | 44.99 | 1.109 | 50 | 0.722 | 0.0001 |
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P-51H TIP | 11.99 | 44.99 | 1.332 | 47.5 | 0.895 | 0.0062 |
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NACA 661-212 | 12 | 44.98 | 1.111 | 50 | 0.986 | 0.0011 |
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NACA 66-210 | 10 | 44.98 | 1.105 | 50 | 0.808 | 0 |
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NACA 662-215 | 14.98 | 44.98 | 1.109 | 50 | 0.915 | 0.0002 |
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