Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| RAF 27 | 9.7 | 30 | 0 | 0 | 0.854 | 0.0057 |
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| RAF 30 | 12.56 | 30 | 0.105 | 0.17 | 1.065 | 0.0004 |
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| RAF 31 | 12.69 | 30 | 2.086 | 50 | 1.43 | 0.0056 |
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| RAF 32 | 12.66 | 30 | 5.067 | 50 | 1.827 | 0.0089 |
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| RAF 33 | 12.7 | 30.03 | 4.663 | 30.03 | 1.501 | 0.0063 |
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