Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| BOEING 707 .08 SPAN | 11.43 | 24 | 0.227 | 6 | 0.918 | 0.0076 |
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| BOEING 737 ROOT AIRFOI | 15.33 | 19.61 | 0.233 | 4.95 | 1.372 | 0.011 |
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| BOEING-VERTOL VR-1 | 10.95 | 35.27 | 1.542 | 43.33 | 1.121 | 0.0059 |
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| CLARK K | 11.38 | 39.65 | 3.245 | 39.65 | 1.676 | 0.0066 |
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| CLARK V | 11.6 | 30 | 3.355 | 50 | 1.617 | 0.0074 |
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