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.

Bibliographic Details
Main Author: Chan, Keen Ian, 1972-
Other Authors: Yifang Gong and Choon S. Tan.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2013
Subjects:
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.
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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
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