Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
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NACA 4510 | 8.01 | 28.39 | 6.438 | 46.85 | 0.741 | 0.0145 |
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NACA 4512 | 12.2 | 26.89 | 3.257 | 51.63 | 1.25 | 0.0059 |
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NACA 63-010 | 9.98 | 35 | 0 | 0 | 0.699 | 0.0065 |
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NACA 631-212 | 11.98 | 34.94 | 1.108 | 50 | 1.071 | 0.0068 |
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NACA 631-412 | 11.98 | 34.88 | 2.215 | 50 | 1.268 | 0.007 |
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