Influence of fuselage and canard-type control surface on the flow field adjacent to a rearward fuselage station at a Mach number of 2.0 : data presentation
| Author: | Obery, Leonard J. |
|---|---|
| Additional Authors: | Fradenburgh, Evan A. |
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E51K05 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59257/ |
