Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA M12 | 11.9 | 30 | 1.942 | 30 | 1.382 | 0.01 |
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| NACA M20 | 8.26 | 30 | 5.939 | 30 | 1.436 | 0.0096 |
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| NACA M6 | 12 | 30 | 2.142 | 30 | 1.34 | 0.0119 |
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| NACA6451.COR | 13.94 | 38.2 | 2.651 | 51.68 | 1.258 | 0.0029 |
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| NASA/AMES A-01 | 10.25 | 30 | 1.368 | 15 | 1.159 | 0.0144 |
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