Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 64A-312 | 11.95 | 38.26 | 1.554 | 51.68 | 1.059 | 0.009 |
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| NACA 64A410 | 9.96 | 38.26 | 2.115 | 51.68 | 1.065 | 0.0009 |
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| NACA 65A-312 | 11.97 | 41.62 | 1.56 | 51.68 | 1.064 | 0.0012 |
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| NACA6451.COR | 13.94 | 38.2 | 2.651 | 51.68 | 1.258 | 0.0029 |
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| EPPLER 214 | 11.1 | 33.08 | 4.032 | 51.99 | 1.517 | 0.0079 |
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