Performance of 19XB-2A Gas Turbine 1 - Effect of Pressure Ratio and Inlet Pressure on Turbine Performance for an Inlet Temperature of 800 Degrees R
| Author: | Kohl, Robert C. |
|---|---|
| Year: | 1946 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E6K18 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc65551/ |