Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| CLARK V | 11.6 | 30 | 3.355 | 50 | 1.617 | 0.0074 |
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| NACA 653-618 | 17.97 | 39.826 | 3.324 | 50 | 1.618 | 0.0085 |
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| ATR | 14.52 | 25.4 | 2.882 | 21.4 | 1.632 | 0.0092 |
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| CLARK W | 11.21 | 30 | 3.684 | 40 | 1.643 | 0.0075 |
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| NACA 4412 | 12.02 | 30 | 3.943 | 40 | 1.649 | 0.0029 |
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V 1.0