Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages IV : modification of aerodynamic design and prediction of performance
| Author: | Geye, Richard P |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E55B28 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61343/ |