Effect of interstage bleed on rotating stall and blade vibration in a 13-stage axial-flow compressor in a turbojet engine
| Author: | Calvert, Howard F. |
|---|---|
| Additional Authors: | Johnson, D. F. |
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E56I06 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62934/ |
