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Cold-air performance of the compressor-drive turbine of the department of energy baseline automobile gas-turbine engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Roelke, R. J. McLallin, K. L. |
| Copyright Year | 1978 |
| Description | The aerodynamic performance of the compressor-drive turbine of the DOE baseline gas-turbine engine was determined over a range of pressure ratios and speeds. In addition, static pressures were measured in the diffusing transition duct located immediately downstream of the turbine. Results are presented in terms of mass flow, torque, specific work, and efficiency for the turbine and in terms of pressure recovery and effectiveness for the transition duct. |
| File Size | 3474458 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780018155 |
| Archival Resource Key | ark:/13960/t9479667w |
| Language | English |
| Publisher Date | 1978-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Static Pressure Turbocompressors Performance Tests Torque Gas Turbine Engines Automobile Engines Aerodynamic Characteristics Mass Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |