Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
---|---|---|---|---|---|---|---|
NACA 663-418 | 17.98 | 44.94 | 2.216 | 50 | 1.394 | 0.0076 |
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NACA 4418 | 18 | 30 | 3.934 | 40 | 1.551 | 0.0104 |
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NACA 0219 | 18.99 | 28.73 | 0 | 0 | 1.427 | 0.013 |
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NACA 23021 | 20.95 | 30 | 1.846 | 10 | 1.121 | 0.0046 |
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NACA 654-221 | 20.98 | 39.93 | 1.113 | 50 | 0.646 | 0.0123 |
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