Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| B-29 ROOT | 21.92 | 29.94 | 1.782 | 39.94 | 1.699 | 0.0333 |
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| NACA 654-221 | 20.98 | 39.93 | 1.113 | 50 | 0.646 | 0.0123 |
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| NACA 664-221 | 20.98 | 44.97 | 1.119 | 50 | 1.434 | 0.008 |
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| NACA 23021 | 20.95 | 30 | 1.846 | 10 | 1.121 | 0.0046 |
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| NACA 0219 | 18.99 | 28.73 | 0 | 0 | 1.427 | 0.013 |
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