Winfoil Airfoils - Total Number: 277
| Name | T/C % | T/C Chord % | Camber % | Camber Chord % | CL Max | CD Min | |
|---|---|---|---|---|---|---|---|
| NASA/LANGLEY SC(2)-0714 | 13.97 | 37 | 2.246 | 81 | 1.52 | 0.0144 |
View
|
| P-51D ROOT (BL17.5) | 16.45 | 38.874 | 1.266 | 68.267 | 1.482 | 0.0063 |
View
|
| P-51D TIP (BL215) | 11.37 | 46.26 | 1.313 | 46.26 | 0.958 | 0.0054 |
View
|
| P-51H ROOT | 15.49 | 44.98 | 1.333 | 47.5 | 1.223 | 0.0031 |
View
|
| P-51H TIP | 11.99 | 44.99 | 1.332 | 47.5 | 0.895 | 0.0062 |
View
|
V 1.0