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Performance of Compressor of XJ-41-V Turbojet Engine 2 - Static-Pressure Ratios and Limitation of Maximum Flow at Equivalent Compressor Speed of 8000 RPM
| Content Provider | University of North Texas |
|---|---|
| Author | Dildine, Dean M. Arthur, W. Lewis |
| Organization | Flight Propulsion Research Laboratory |
| Description | "At the request of the Air Material Command, Army Air Forces, an investigation was conducted by the NACA Cleveland laboratory to determine the performance characteristics of the compressor of the XJ-41-V turbojet engine. This report is the second in a series presenting the compressor performance and analysis of flow conditions in the compressor. The static-pressure variation in the direction of flow through the compressor and the location and the cause of the maximum flow restriction at an equivalent speed of 8000 rpm are presented" (p. 1). |
| File Format | |
| Archival Resource Key | ark:/67531/metadc65002 |
| Language | English |
| Publisher Date | 2019-03-14 |
| Access Restriction | Open |
| Subject Keyword | XJ-41-V turbojet engine aircraft engines aircraft power |
| Content Type | Text |
| Resource Type | Report |
