Investigation of translating-spike supersonic inlet as means of mass-flow control at Mach numbers of 1.5, 1.8, and 2.0
| Author: | Gorton, Gerald C. |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E53G10 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59636/ |