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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| S.I. 53009 | 9.07 | 30 | 5.007 | 30 | 1.178 | 0.009 |
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| RAF 32 | 12.66 | 30 | 5.067 | 50 | 1.827 | 0.0089 |
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| MILEY | 12.86 | 35.03 | 5.132 | 35.03 | 1.43 | 0.005 |
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| EPPLER 62 (5.62%) | 5.66 | 26.238 | 5.307 | 49.334 | 1.302 | 0.0058 |
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