Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| EPPLER 61 | 6.15 | 30 | 6.517 | 50 | 1.149 | 0.0005 |
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| NACA 64A410 | 9.96 | 38.26 | 2.115 | 51.68 | 1.065 | 0.0009 |
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| NACA 661-212 | 12 | 44.98 | 1.111 | 50 | 0.986 | 0.0011 |
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| NACA 65A-312 | 11.97 | 41.62 | 1.56 | 51.68 | 1.064 | 0.0012 |
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| EPPLER 378 | 4.08 | 10.36 | 8.109 | 35.92 | 1.686 | 0.0014 |
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