Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
---|---|---|---|---|---|---|---|
NACA 6409 | 9.04 | 50 | 5.973 | 40 | 1.383 | 0 |
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NACA 6412 | 12.06 | 50 | 5.981 | 40 | 1.535 | 0.0075 |
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NACA 64A210 | 9.97 | 39.96 | 1.325 | 49.99 | 0.558 | 0.0004 |
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NACA 64A-312 | 11.95 | 38.26 | 1.554 | 51.68 | 1.059 | 0.009 |
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NACA 64A410 | 9.96 | 38.26 | 2.115 | 51.68 | 1.065 | 0.0009 |
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