Experimental investigation of an axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers III : blade-row performance of stage with transonic rotor and subsonic stator at corrected tip speeds of 800 and 1000 feet per secon
| Author: | Schwenk, Francis C |
|---|---|
| Additional Authors: | Lieblein, Seymour |
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E53G17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59687/ |