Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| P-51H ROOT | 15.49 | 44.98 | 1.333 | 47.5 | 1.223 | 0.0031 |
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| NACA 0016 | 15.91 | 27.3202 | 0 | 0 | 1.332 | 0.0106 |
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| S8037 | 15.98 | 33.47 | 2.431 | 36.9 | 1.574 | 0.005 |
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| S8036 | 15.99 | 36.85 | 1.825 | 36.85 | 1.538 | 0.005 |
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| S8036 (16%) | 16 | 36.848 | 1.821 | 36.848 | 1.538 | 0.0054 |
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