Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
---|---|---|---|---|---|---|---|
NACA 63-010 | 9.98 | 35 | 0 | 0 | 0.699 | 0.0065 |
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EPPLER 184 | 8.31 | 32.12 | 1.146 | 36.76 | 0.7 | 0.005 |
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NACA 66-209 | 8.98 | 44.99 | 1.109 | 50 | 0.722 | 0.0001 |
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MH 22 | 7.2 | 28.86 | 1.89 | 33.42 | 0.725 | 0.0048 |
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MH22 | 7.21 | 28.86 | 1.889 | 33.42 | 0.739 | 0.0041 |
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