Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
---|---|---|---|---|---|---|---|
NACA 652-415 | 14.98 | 39.9 | 2.218 | 50 | 1.248 | 0.0026 |
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NACA 653-218 | 17.97 | 39.94 | 1.118 | 50 | 1.172 | 0.0034 |
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NACA 653-418 | 17.97 | 39.88 | 2.221 | 50 | 1.41 | 0.0082 |
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NACA 653-618 | 17.97 | 39.826 | 3.324 | 50 | 1.618 | 0.0085 |
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NACA 654-221 | 20.98 | 39.93 | 1.113 | 50 | 0.646 | 0.0123 |
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