Effects on the weight-flow range and efficiency of a typical axial-flow compressor inlet stage that result from the use of a decreased blade camber or decreased guide-vane turning
| Author: | Jackson, Robert J. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E52G02 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59339/ |