Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 0219 | 18.99 | 28.73 | 0 | 0 | 1.427 | 0.013 |
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| NACA 23018 | 17.96 | 30 | 1.835 | 15 | 1.275 | 0.0132 |
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| GOTTINGEN 398 | 13.75 | 30 | 4.409 | 40 | 1.815 | 0.0136 |
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| NASA/AMES A-01 | 10.25 | 30 | 1.368 | 15 | 1.159 | 0.0144 |
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| NASA/LANGLEY SC(2)-0714 | 13.97 | 37 | 2.246 | 81 | 1.52 | 0.0144 |
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