Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| CLARK W | 11.21 | 30 | 3.684 | 40 | 1.643 | 0.0075 |
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| CLARK Y | 11.73 | 30.87 | 3.528 | 43.47 | 1.595 | 0.006 |
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| CLARK YH | 11.9 | 30 | 2.45 | 30 | 1.392 | 0.0095 |
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| CLARK YS | 11.7 | 30 | 2.353 | 30 | 1.274 | 0.0055 |
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| DAE51 | 9.38 | 30.94 | 3.465 | 46.07 | 1.186 | 0.0078 |
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