An assessment of computational procedures for eleven-stage compressor response to inlet distortion
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.
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Format: | Thesis |
Language: | eng |
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Massachusetts Institute of Technology
2013
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Online Access: | http://hdl.handle.net/1721.1/82766 |
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author | Chan, Keen Ian, 1972- |
author2 | Yifang Gong and Choon S. Tan. |
author_facet | Yifang Gong and Choon S. Tan. Chan, Keen Ian, 1972- |
author_sort | Chan, Keen Ian, 1972- |
collection | MIT |
description | Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003. |
first_indexed | 2024-09-23T14:58:01Z |
format | Thesis |
id | mit-1721.1/82766 |
institution | Massachusetts Institute of Technology |
language | eng |
last_indexed | 2024-09-23T14:58:01Z |
publishDate | 2013 |
publisher | Massachusetts Institute of Technology |
record_format | dspace |
spelling | mit-1721.1/827662019-04-11T11:31:52Z An assessment of computational procedures for eleven-stage compressor response to inlet distortion Chan, Keen Ian, 1972- Yifang Gong and Choon S. Tan. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003. Includes bibliographical references (p. 74-76). by Keen Ian Chan. S.M. 2013-12-06T20:39:59Z 2013-12-06T20:39:59Z 2003 2003 Thesis http://hdl.handle.net/1721.1/82766 54070371 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 76 p. application/pdf Massachusetts Institute of Technology |
spellingShingle | Aeronautics and Astronautics. Chan, Keen Ian, 1972- An assessment of computational procedures for eleven-stage compressor response to inlet distortion |
title | An assessment of computational procedures for eleven-stage compressor response to inlet distortion |
title_full | An assessment of computational procedures for eleven-stage compressor response to inlet distortion |
title_fullStr | An assessment of computational procedures for eleven-stage compressor response to inlet distortion |
title_full_unstemmed | An assessment of computational procedures for eleven-stage compressor response to inlet distortion |
title_short | An assessment of computational procedures for eleven-stage compressor response to inlet distortion |
title_sort | assessment of computational procedures for eleven stage compressor response to inlet distortion |
topic | Aeronautics and Astronautics. |
url | http://hdl.handle.net/1721.1/82766 |
work_keys_str_mv | AT chankeenian1972 anassessmentofcomputationalproceduresforelevenstagecompressorresponsetoinletdistortion AT chankeenian1972 assessmentofcomputationalproceduresforelevenstagecompressorresponsetoinletdistortion |