Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers I : rotor design and over-all performance at tip speeds from 60 to 100 percent of design
| Author: | Serovy, George K |
|---|---|
| Additional Authors: | Robbins, William H |
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E53I11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59984/ |