Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| P-51D ROOT (BL17.5) | 16.45 | 38.874 | 1.266 | 68.267 | 1.482 | 0.0063 |
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| EPPLER 1200 | 16.93 | 36.11 | 3.48 | 40.77 | 1.818 | 0.0072 |
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| EPPLER 266 | 17.3 | 39.79 | 3.062 | 39.79 | 1.483 | 0.0066 |
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| NACA 65-218 | 17.95 | 39.95 | 1.123 | 50 | 1.399 | 0.0076 |
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| NACA 23018 | 17.96 | 30 | 1.835 | 15 | 1.275 | 0.0132 |
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