Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
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NACA 63-206 | 5.99 | 34.97 | 1.108 | 50 | 0.62 | 0.0052 |
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NACA 63-209 | 8.99 | 34.96 | 1.11 | 50 | 0.756 | 0.006 |
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NACA 63-210 | 9.98 | 34.95 | 1.11 | 50 | 0.961 | 0.0061 |
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NACA 632-215 | 14.97 | 34.93 | 1.114 | 50 | 0.998 | 0.0052 |
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NACA 632-415 | 14.98 | 34.85 | 2.213 | 50 | 1.268 | 0.0028 |
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