Effect of an Adjustable Supersonic Inlet on the Performance Up to Mach Number 2.0 of a J34 Turbojet Engine
| Author: | Beke, Andrew |
|---|---|
| Additional Authors: | Englert, Gerald |
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E55I27 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61692/ |