Effect of airfoil section and tip tanks on the aerodynamic characteristics at high subsonic speeds of an unswept wing of aspect ratio 5.16 and taper ratio 0.61
| Author: | Silvers, H. Norman |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9J04 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58332/ |