Experimental investigation of an axial-flow-compressor inlet stage operating at transonic relative inlet Mach numbers V : rotor blade-element performance at a reduced blade angle
| Author: | Schwenk, Francis C |
|---|---|
| Additional Authors: | Lewis, George W , Jr |
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E56J17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62950/ |