The effect of tip tanks on the rolling characteristics at high subsonic Mach numbers of a wing having an aspect ratio of 3 with quarter-chord line swept back 35 degrees
| Author: | Kuhn, Richard E |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9J19 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58416/ |