Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
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AG 10 | 10 | 15.999 | 6.443 | 32.1 | 1.798 | 0.015 |
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GOTTINGEN 398 | 13.75 | 30 | 4.409 | 40 | 1.815 | 0.0136 |
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EPPLER 1200 | 16.93 | 36.11 | 3.48 | 40.77 | 1.818 | 0.0072 |
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RAF 32 | 12.66 | 30 | 5.067 | 50 | 1.827 | 0.0089 |
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RAF 6 | 9.97 | 29.97 | 4.541 | 29.97 | 1.996 | 0.0078 |
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