Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 65-912 | 11.96 | 41.52 | 4.861 | 50 | 1.5 | 0.0046 |
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| NACA 65A-312 | 11.97 | 41.62 | 1.56 | 51.68 | 1.064 | 0.0012 |
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| NACA 65A-410 | 9.97 | 41.61 | 2.125 | 50 | 1.032 | 0.007 |
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| NACA 661-212 | 12 | 44.98 | 1.111 | 50 | 0.986 | 0.0011 |
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| NACA 66-206 | 6 | 44.99 | 1.107 | 50 | 0.688 | 0.0003 |
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