Stalled flow performance of a single stage transonic compressor
Originally presented as the first author's thesis, M.S. in the M.I.T. Dept. of Mechanical Engineering, 1978
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| Format: | Technical Report |
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Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine & Plasma Dynamics Laboratory, [1978]
2016
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| Online Access: | http://hdl.handle.net/1721.1/104421 |
| _version_ | 1826216674416656384 |
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| author | Bartlett, Frederick Girard Greitzer, E. M. (Edward M.), 1941- |
| author2 | Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory |
| author_facet | Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory Bartlett, Frederick Girard Greitzer, E. M. (Edward M.), 1941- |
| author_sort | Bartlett, Frederick Girard |
| collection | MIT |
| description | Originally presented as the first author's thesis, M.S. in the M.I.T. Dept. of Mechanical Engineering, 1978 |
| first_indexed | 2024-09-23T16:51:17Z |
| format | Technical Report |
| id | mit-1721.1/104421 |
| institution | Massachusetts Institute of Technology |
| last_indexed | 2024-09-23T16:51:17Z |
| publishDate | 2016 |
| publisher | Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine & Plasma Dynamics Laboratory, [1978] |
| record_format | dspace |
| spelling | mit-1721.1/1044212019-04-12T16:13:20Z Stalled flow performance of a single stage transonic compressor Bartlett, Frederick Girard Greitzer, E. M. (Edward M.), 1941- Massachusetts Institute of Technology. Gas Turbine and Plasma Dynamics Laboratory TJ778.M41 G24 no.144 Compressors -- Aerodynamics Aerodynamics, Transonic Originally presented as the first author's thesis, M.S. in the M.I.T. Dept. of Mechanical Engineering, 1978 Includes bibliographical references (page 48) The stalled flow performance of a single stage transonic compressor is examined, using data from the MIT Gas Turbine Laboratory's Blowdown Compressor Facility. Measurements of the blowdown corrected weightflow are included, as well as stage exit static to inlet total pressure rise, and rotating stall cell measurements. A comparison of the flow blockage, as represented by stall cell circumferential extent, with the blowdown corrected weightflow is made. The 100% design speed stalled flow performance characteristic is presented. Radial traverse.data is also presented including flow angles, static and total pressures, and Mach number components. Supported by the NASA Lewis Research Center grant NGL 22-009-383 2016-09-27T19:59:06Z 2016-09-27T19:59:06Z 1978 Technical Report http://hdl.handle.net/1721.1/104421 06550418 GT & PDL report ; no. 144 79 pages application/pdf Cambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine & Plasma Dynamics Laboratory, [1978] |
| spellingShingle | TJ778.M41 G24 no.144 Compressors -- Aerodynamics Aerodynamics, Transonic Bartlett, Frederick Girard Greitzer, E. M. (Edward M.), 1941- Stalled flow performance of a single stage transonic compressor |
| title | Stalled flow performance of a single stage transonic compressor |
| title_full | Stalled flow performance of a single stage transonic compressor |
| title_fullStr | Stalled flow performance of a single stage transonic compressor |
| title_full_unstemmed | Stalled flow performance of a single stage transonic compressor |
| title_short | Stalled flow performance of a single stage transonic compressor |
| title_sort | stalled flow performance of a single stage transonic compressor |
| topic | TJ778.M41 G24 no.144 Compressors -- Aerodynamics Aerodynamics, Transonic |
| url | http://hdl.handle.net/1721.1/104421 |
| work_keys_str_mv | AT bartlettfrederickgirard stalledflowperformanceofasinglestagetransoniccompressor AT greitzeremedwardm1941 stalledflowperformanceofasinglestagetransoniccompressor |