Investigation of the effect of velocity diagram on inlet total-pressure distortions through single-stage subsonic axial-flow compressors
| Author: | Ashby, George C , Jr |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L57A03 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63459/ |