Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 663-218 | 17.97 | 44.97 | 1.117 | 50 | 1.166 | 0.0073 |
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| NACA 23018 | 17.96 | 30 | 1.835 | 15 | 1.275 | 0.0132 |
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| NACA 2418 | 17.96 | 30 | 1.95 | 40 | 1.367 | 0.0128 |
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| NACA 65-218 | 17.95 | 39.95 | 1.123 | 50 | 1.399 | 0.0076 |
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| EPPLER 266 | 17.3 | 39.79 | 3.062 | 39.79 | 1.483 | 0.0066 |
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