Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 4418 | 18 | 30 | 3.934 | 40 | 1.551 | 0.0104 |
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| NACA 663-418 | 17.98 | 44.94 | 2.216 | 50 | 1.394 | 0.0076 |
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| NACA 653-218 | 17.97 | 39.94 | 1.118 | 50 | 1.172 | 0.0034 |
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| NACA 653-418 | 17.97 | 39.88 | 2.221 | 50 | 1.41 | 0.0082 |
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| NACA 653-618 | 17.97 | 39.826 | 3.324 | 50 | 1.618 | 0.0085 |
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