Design of the MIT Breakdown Turbine Facility
April 1985
| Main Authors: | , , |
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| Other Authors: | |
| Format: | Technical Report |
| Published: |
Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1985]
2016
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| Subjects: | |
| Online Access: | http://hdl.handle.net/1721.1/104724 |
| _version_ | 1811095007549980672 |
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| author | Epstein, Alan H. (Alan Henry) Guenette, Gerald R. (Gerald Roger) Norton, Robert J. G. |
| author2 | Massachusetts Institute of Technology. Gas Turbine Laboratory |
| author_facet | Massachusetts Institute of Technology. Gas Turbine Laboratory Epstein, Alan H. (Alan Henry) Guenette, Gerald R. (Gerald Roger) Norton, Robert J. G. |
| author_sort | Epstein, Alan H. (Alan Henry) |
| collection | MIT |
| description | April 1985 |
| first_indexed | 2024-09-23T16:09:03Z |
| format | Technical Report |
| id | mit-1721.1/104724 |
| institution | Massachusetts Institute of Technology |
| last_indexed | 2024-09-23T16:09:03Z |
| publishDate | 2016 |
| publisher | Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1985] |
| record_format | dspace |
| spelling | mit-1721.1/1047242019-04-10T12:33:58Z Design of the MIT Breakdown Turbine Facility Design of the Massachusetts Institute of Technology Breakdown Turbine Facility Epstein, Alan H. (Alan Henry) Guenette, Gerald R. (Gerald Roger) Norton, Robert J. G. Massachusetts Institute of Technology. Gas Turbine Laboratory TJ778.M41 G24 no.183 Airplanes -- Motors Heat -- Transmission April 1985 Includes bibliographical references (page 151) Summary: This report details the design, construction, and preliminary testing of a short duration (0.4 sec) test facility capable of testing 0.5 meter diameter, film cooled, high work aircraft turbine stages under conditions which rigorously simulate actual engine conditions. The simulation capability of the facility extends up to 40 atm inlet pressure at 2500 0K (40000F) turbine inlet temperatures. The facility is intended primarily for the exploration of unsteady, three-dimensional fluid mechanics and heat transfer in modern turbine stages. "This research was sponsored by the Office of Naval Research, Mr. Keith Ellingsworth technical monitor, and by Rolls-Royce, Inc." 2016-10-06T21:22:12Z 2016-10-06T21:22:12Z 1985 Technical Report http://hdl.handle.net/1721.1/104724 16206191 GTL report #183 156 pages application/pdf Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1985] |
| spellingShingle | TJ778.M41 G24 no.183 Airplanes -- Motors Heat -- Transmission Epstein, Alan H. (Alan Henry) Guenette, Gerald R. (Gerald Roger) Norton, Robert J. G. Design of the MIT Breakdown Turbine Facility |
| title | Design of the MIT Breakdown Turbine Facility |
| title_full | Design of the MIT Breakdown Turbine Facility |
| title_fullStr | Design of the MIT Breakdown Turbine Facility |
| title_full_unstemmed | Design of the MIT Breakdown Turbine Facility |
| title_short | Design of the MIT Breakdown Turbine Facility |
| title_sort | design of the mit breakdown turbine facility |
| topic | TJ778.M41 G24 no.183 Airplanes -- Motors Heat -- Transmission |
| url | http://hdl.handle.net/1721.1/104724 |
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