Analysis of Limitations Imposed on One-Spool Turboprop-Engine Designs by Compressors and Turbines at Flight Mach Numbers of 0.06, and 0.8
| Author: | Cavicchi, Richard H. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E56I05 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62919/ |