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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| AG08 | 5.83 | 14.2151 | 1.934 | 26.7002 | 0.907 | 0.007 |
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| RAF 15 | 6.45 | 15 | 2.564 | 30 | 1.282 | 0.0059 |
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| RAF 19 | 10.52 | 15 | 10.065 | 40 | 2.23 | 0.0084 |
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| AG09 | 4.86 | 15.9674 | 1.795 | 33.2344 | 0.886 | 0.0096 |
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