Experimental investigation of an axial flow compressor inlet stage operating at transonic relative inlet Mach numbers I : over-all performance of stage with transonic rotor and subsonic stators up to rotor relative inlet Mach number of 1.1
| Author: | Lieblein, Seymour |
|---|---|
| Additional Authors: | Lewis, George W , Jr |
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E52A24 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59093/ |