Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
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NACA 2213 | 12.93 | 27.3499 | 1.987 | 20.6285 | 1.452 | 0.0095 |
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NACA 23012 | 11.97 | 30 | 1.835 | 15 | 1.173 | 0.0072 |
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NACA 23015 | 14.97 | 30 | 1.831 | 15 | 1.48 | 0.0116 |
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NACA 23018 | 17.96 | 30 | 1.835 | 15 | 1.275 | 0.0132 |
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NACA 23021 | 20.95 | 30 | 1.846 | 10 | 1.121 | 0.0046 |
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