Pressure Recovery at Supersonic Speeds Through Annular Duct Inlets Situated in a Region of Appreciable Boundary Layer 2: Effect of an Oblique Shock Wave Immediately Ahead of the Inlet
| Author: | Brajnikoff, George B. |
|---|---|
| Year: | 1948 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A8F08 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57700/ |