Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| BOEING 707 .08 SPAN | 11.43 | 24 | 0.227 | 6 | 0.918 | 0.0076 |
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| NACA 1111 | 10.99 | 31.65 | 0.996 | 9.52 | 0.937 | 0.0095 |
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| NACA 23021 | 20.95 | 30 | 1.846 | 10 | 1.121 | 0.0046 |
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| MH53 | 9.43 | 38.33 | 0.416 | 14.96 | 0.558 | 0.0056 |
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| NACA 23012 | 11.97 | 30 | 1.835 | 15 | 1.173 | 0.0072 |
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