Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 64A-510 | 9.96 | 38.24 | 2.665 | 50 | 1.167 | 0.0045 |
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| NACA 651-212 | 11.98 | 39.96 | 1.116 | 50 | 0.637 | 0.0041 |
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| NACA 651-412 | 11.98 | 39.92 | 2.215 | 50 | 1.205 | 0.0025 |
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| NACA 65-218 | 17.95 | 39.95 | 1.123 | 50 | 1.399 | 0.0076 |
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| NACA 652-215 | 14.97 | 39.95 | 1.115 | 50 | 0.958 | 0.0054 |
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