Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 663-418 | 17.98 | 44.94 | 2.216 | 50 | 1.394 | 0.0076 |
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| NACA 664-221 | 20.98 | 44.97 | 1.119 | 50 | 1.434 | 0.008 |
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| NACA 671-215 | 14.98 | 50 | 1.111 | 50 | 0.803 | 0.0001 |
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| NACA 747A315 | 14.97 | 40.2 | 2.531 | 35 | 1.2 | 0.0102 |
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| NACA 747A415 | 14.98 | 40.18 | 3.048 | 34.96 | 1.297 | 0.0076 |
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