Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 671-215 | 14.98 | 50 | 1.111 | 50 | 0.803 | 0.0001 |
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| NACA 662-215 | 14.98 | 44.98 | 1.109 | 50 | 0.915 | 0.0002 |
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| NACA 66-206 | 6 | 44.99 | 1.107 | 50 | 0.688 | 0.0003 |
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| NACA 64A210 | 9.97 | 39.96 | 1.325 | 49.99 | 0.558 | 0.0004 |
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| RAF 30 | 12.56 | 30 | 0.105 | 0.17 | 1.065 | 0.0004 |
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