Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| ARA-D 10% | 10.01 | 25 | 3.724 | 35 | 1.741 | 0.0202 |
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| ARA-D 13% | 13 | 25 | 3.34 | 30 | 1.713 | 0.0247 |
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| ARA-D 6% | 6.04 | 20 | 4.752 | 45 | 1.552 | 0.0145 |
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| ATR | 14.52 | 25.4 | 2.882 | 21.4 | 1.632 | 0.0092 |
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| B-29 ROOT | 21.92 | 29.94 | 1.782 | 39.94 | 1.699 | 0.0333 |
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