Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.
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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/1721.1/82227 |
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author | Lenglin, Geoffroy (Geoffroy Philippe), 1976- |
author2 | Choon S. Tan. |
author_facet | Choon S. Tan. Lenglin, Geoffroy (Geoffroy Philippe), 1976- |
author_sort | Lenglin, Geoffroy (Geoffroy Philippe), 1976- |
collection | MIT |
description | Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002. |
first_indexed | 2024-09-23T13:46:57Z |
format | Thesis |
id | mit-1721.1/82227 |
institution | Massachusetts Institute of Technology |
language | eng |
last_indexed | 2024-09-23T13:46:57Z |
publishDate | 2013 |
publisher | Massachusetts Institute of Technology |
record_format | dspace |
spelling | mit-1721.1/822272019-04-12T11:22:06Z Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment Lenglin, Geoffroy (Geoffroy Philippe), 1976- 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, 2002. Includes bibliographical references (p. 90-91). by Geoffroy Lenglin. S.M. 2013-11-18T18:57:05Z 2013-11-18T18:57:05Z 2002 2002 Thesis http://hdl.handle.net/1721.1/82227 51276747 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 91 p. application/pdf Massachusetts Institute of Technology |
spellingShingle | Aeronautics and Astronautics. Lenglin, Geoffroy (Geoffroy Philippe), 1976- Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment |
title | Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment |
title_full | Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment |
title_fullStr | Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment |
title_full_unstemmed | Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment |
title_short | Characterization of wake- and tip-vortex-induced unsteady blade response in multistage compressor environment |
title_sort | characterization of wake and tip vortex induced unsteady blade response in multistage compressor environment |
topic | Aeronautics and Astronautics. |
url | http://hdl.handle.net/1721.1/82227 |
work_keys_str_mv | AT lenglingeoffroygeoffroyphilippe1976 characterizationofwakeandtipvortexinducedunsteadybladeresponseinmultistagecompressorenvironment |