Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| ARA-D 6% | 6.04 | 20 | 4.752 | 45 | 1.552 | 0.0145 |
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| NACA 4510 | 8.01 | 28.39 | 6.438 | 46.85 | 0.741 | 0.0145 |
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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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| GOTTINGEN 398 | 13.75 | 30 | 4.409 | 40 | 1.815 | 0.0136 |
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