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Turbine for ordnance turbojet engine. 2: cold-air performance with opened stator
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nusbaum, W. J. Haas, J. E. Kofskey, M. G. |
| Copyright Year | 1974 |
| Description | A single-stage axial-flow turbine was investigated to determine the effect of increased stator throat area on the performance level of a turbojet engine turbine. The stator blades were bent to increase the throat area in order to move the compressor operating point in the engine farther away from surge. Results are compared with those obtained with the as-cast stator setting. |
| File Size | 3055044 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740019165 |
| Archival Resource Key | ark:/13960/t4dn8x462 |
| Language | English |
| Publisher Date | 1974-06-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Air Flow Axial Flow Turbines Propulsion System Performance Engine Tests Power Efficiency Cold Flow Tests Propulsion System Configurations Turbojet Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
