Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| 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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| NACA 0219 | 18.99 | 28.73 | 0 | 0 | 1.427 | 0.013 |
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| NACA 63-010 | 9.98 | 35 | 0 | 0 | 0.699 | 0.0065 |
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| RAF 27 | 9.7 | 30 | 0 | 0 | 0.854 | 0.0057 |
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