Investigation of a supersonic-inlet - turbojet-engine combination at Mach 2.0 and angles of attack up to 6 degrees
| Author: | Hearth, Donald P. |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E57D18 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63540/ |