Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 23015 | 14.97 | 30 | 1.831 | 15 | 1.48 | 0.0116 |
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| NACA 23018 | 17.96 | 30 | 1.835 | 15 | 1.275 | 0.0132 |
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| NASA/AMES A-01 | 10.25 | 30 | 1.368 | 15 | 1.159 | 0.0144 |
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| EPPLER 325 | 12.61 | 30.45 | 1.812 | 18.29 | 0.845 | 0.0209 |
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| NACA 2213 | 12.93 | 27.3499 | 1.987 | 20.6285 | 1.452 | 0.0095 |
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