Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 4510 | 8.01 | 28.39 | 6.438 | 46.85 | 0.741 | 0.0145 |
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| S.I. 64009 | 9.23 | 30 | 6.045 | 40 | 1.515 | 0.0093 |
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| NACA 6412 | 12.06 | 50 | 5.981 | 40 | 1.535 | 0.0075 |
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| NACA 6409 | 9.04 | 50 | 5.973 | 40 | 1.383 | 0 |
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| NACA M20 | 8.26 | 30 | 5.939 | 30 | 1.436 | 0.0096 |
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