Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| AG08 | 5.83 | 14.2151 | 1.934 | 26.7002 | 0.907 | 0.007 |
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| AG13 | 5.83 | 21.2982 | 2.209 | 28.1134 | 0.887 | 0.0074 |
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| AG18 | 5.87 | 20.705 | 2.158 | 42.7408 | 0.982 | 0.0064 |
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| NACA 63-206 | 5.99 | 34.97 | 1.108 | 50 | 0.62 | 0.0052 |
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| NACA 66-206 | 6 | 44.99 | 1.107 | 50 | 0.688 | 0.0003 |
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