Winfoil Airfoils - Total Number: 277
Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
---|---|---|---|---|---|---|---|
CLARK K | 11.38 | 39.65 | 3.245 | 39.65 | 1.676 | 0.0066 |
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EPPLER 378 | 4.08 | 10.36 | 8.109 | 35.92 | 1.686 | 0.0014 |
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B-29 ROOT | 21.92 | 29.94 | 1.782 | 39.94 | 1.699 | 0.0333 |
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GOTTINGE.COR | 13.75 | 30 | 4.409 | 40 | 1.699 | 0.016 |
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GOTTINGEN 549 | 13.83 | 30 | 4.688 | 40 | 1.706 | 0.0084 |
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