Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 632-415 | 14.98 | 34.85 | 2.213 | 50 | 1.268 | 0.0028 |
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| NACA 4412 | 12.02 | 30 | 3.943 | 40 | 1.649 | 0.0029 |
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| NACA6451.COR | 13.94 | 38.2 | 2.651 | 51.68 | 1.258 | 0.0029 |
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| P-51H ROOT | 15.49 | 44.98 | 1.333 | 47.5 | 1.223 | 0.0031 |
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| S7012 | 8.75 | 27.74 | 1.963 | 38.07 | 1.024 | 0.0032 |
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