Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| EPPLER 378 | 4.08 | 10.36 | 8.109 | 35.92 | 1.686 | 0.0014 |
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| CLARK K | 11.38 | 39.65 | 3.245 | 39.65 | 1.676 | 0.0066 |
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| NACA 4412 | 12.02 | 30 | 3.943 | 40 | 1.649 | 0.0029 |
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| CLARK W | 11.21 | 30 | 3.684 | 40 | 1.643 | 0.0075 |
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| ATR | 14.52 | 25.4 | 2.882 | 21.4 | 1.632 | 0.0092 |
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