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Active control of rotating stall in a transonic compressor stage with inlet distortion

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dc.contributor.advisor James D. Paduano. en_US
dc.contributor.author Spakovszky, Zoltán S. (Zoltán Sándor), 1972- en_US
dc.date.accessioned 2010-01-07T20:48:48Z
dc.date.available 2010-01-07T20:48:48Z
dc.date.copyright 1999 en_US
dc.date.issued 1999 en_US
dc.identifier.uri http://hdl.handle.net/1721.1/50522
dc.description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1999. en_US
dc.description Includes bibliographical references (p. 101-103). en_US
dc.description.statementofresponsibility by Zoltán S. Spakovszky. en_US
dc.format.extent 103 p. en_US
dc.language.iso eng en_US
dc.publisher Massachusetts Institute of Technology en_US
dc.rights 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. en_US
dc.rights.uri http://dspace.mit.edu/handle/1721.1/7582 en_US
dc.subject Aeronautics and Astronautics en_US
dc.title Active control of rotating stall in a transonic compressor stage with inlet distortion en_US
dc.type Thesis en_US
dc.description.degree S.M. en_US
dc.contributor.department Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics en_US
dc.identifier.oclc 42695842 en_US


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