| dc.contributor.author | Epstein, Alan H. (Alan Henry) | en_US |
| dc.contributor.author | Guenette, Gerald R. (Gerald Roger) | en_US |
| dc.contributor.author | Norton, Robert J. G. | en_US |
| dc.contributor.other | Massachusetts Institute of Technology. Gas Turbine Laboratory | en_US |
| dc.date.accessioned | 2016-10-06T21:22:12Z | |
| dc.date.available | 2016-10-06T21:22:12Z | |
| dc.date.issued | 1985 | en_US |
| dc.identifier.uri | http://hdl.handle.net/1721.1/104724 | |
| dc.description | April 1985 | en_US |
| dc.description | Includes bibliographical references (page 151) | en_US |
| dc.description.abstract | 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. | en_US |
| dc.description.sponsorship | "This research was sponsored by the Office of Naval Research, Mr. Keith Ellingsworth technical monitor, and by Rolls-Royce, Inc." | en_US |
| dc.format.extent | 156 pages | en_US |
| dc.publisher | Cambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1985] | en_US |
| dc.relation.ispartofseries | GTL report #183 | en_US |
| dc.subject.lcc | TJ778.M41 G24 no.183 | en_US |
| dc.subject.lcsh | Airplanes -- Motors | en_US |
| dc.subject.lcsh | Heat -- Transmission | en_US |
| dc.title | Design of the MIT Breakdown Turbine Facility | en_US |
| dc.title.alternative | Design of the Massachusetts Institute of Technology Breakdown Turbine Facility | en_US |
| dc.type | Technical Report | en_US |
| dc.identifier.oclc | 16206191 | en_US |
