Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NACA 66-209 | 8.98 | 44.99 | 1.109 | 50 | 0.722 | 0.0001 |
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| NACA 66-210 | 10 | 44.98 | 1.105 | 50 | 0.808 | 0 |
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| NACA 662-215 | 14.98 | 44.98 | 1.109 | 50 | 0.915 | 0.0002 |
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| NACA 662-415 | 14.99 | 44.95 | 2.217 | 50 | 0.751 | 0.0001 |
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| NACA 663-218 | 17.97 | 44.97 | 1.117 | 50 | 1.166 | 0.0073 |
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