The Effect of the Inlet Mach Number and Inlet-Boundary-Layer Thickness on the Performance of a 23 Degree Conical-Diffuser-Tail-Pipe Combination
| Author: | Persh, Jerome |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9K10 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62843/ |