Internal performance of a series of circular auxiliary-air inlets immersed in a turbulent boundary layer : Mach number range: 1.5 to 2.0
| Author: | Simon, Paul C |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E54L03 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61091/ |