Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 65A-312 | 11.97 | 41.62 | 1.56 | 51.68 | 1.064 | 0.0012 |
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| NACA6451.COR | 13.94 | 38.2 | 2.651 | 51.68 | 1.258 | 0.0029 |
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| NACA 4512 | 12.2 | 26.89 | 3.257 | 51.63 | 1.25 | 0.0059 |
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| CLARK V | 11.6 | 30 | 3.355 | 50 | 1.617 | 0.0074 |
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| EPPLER 61 | 6.15 | 30 | 6.517 | 50 | 1.149 | 0.0005 |
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