Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 0009 | 8.97 | 30 | 0 | 0 | 0.871 | 0.0065 |
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| NACA 0010 | 9.97 | 30 | 0 | 0 | 0.877 | 0.0016 |
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| NACA 0012 | 11.96 | 30 | 0 | 0 | 1.108 | 0.0092 |
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| NACA 0015 | 15.01 | 28.73 | 0 | 0 | 1.287 | 0.0064 |
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| NACA 0016 | 15.91 | 27.3202 | 0 | 0 | 1.332 | 0.0106 |
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