Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 664-221 | 20.98 | 44.97 | 1.119 | 50 | 1.434 | 0.008 |
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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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| P-51H ROOT | 15.49 | 44.98 | 1.333 | 47.5 | 1.223 | 0.0031 |
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