Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| P-51H ROOT | 15.49 | 44.98 | 1.333 | 47.5 | 1.223 | 0.0031 |
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| NACA 663-218 | 17.97 | 44.97 | 1.117 | 50 | 1.166 | 0.0073 |
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| NACA 664-221 | 20.98 | 44.97 | 1.119 | 50 | 1.434 | 0.008 |
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| NACA 662-415 | 14.99 | 44.95 | 2.217 | 50 | 0.751 | 0.0001 |
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| NACA 663-418 | 17.98 | 44.94 | 2.216 | 50 | 1.394 | 0.0076 |
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