The effects of centrally mounted wing-tip tanks on the subsonic aerodynamic characteristics of a wing of aspect ratio 10 with 35 degrees of sweepback
| Author: | Tinling, Bruce E. |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A50K15 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58752/ |