Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 653-618 | 17.97 | 39.826 | 3.324 | 50 | 1.618 | 0.0085 |
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| CLARK V | 11.6 | 30 | 3.355 | 50 | 1.617 | 0.0074 |
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| CLARK Y | 11.73 | 30.87 | 3.528 | 43.47 | 1.595 | 0.006 |
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| S4180 | 9.8 | 26.13 | 4.49 | 34.8 | 1.589 | 0.0076 |
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| NACA 4415 | 14.99 | 30 | 3.939 | 40 | 1.588 | 0.0058 |
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