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Blade passage flow structure effects on axial compressor rotating stall inception

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dc.contributor.advisor Edward M. Greitzer. en_US Hoying, Donald Andrew en_US 2005-08-18T17:20:39Z 2005-08-18T17:20:39Z 1996 en_US 1996 en_US
dc.description Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996. en_US
dc.description Includes bibliographical references (p. 125-130). en_US
dc.description.statementofresponsibility by Donald Andrew Hoying. en_US
dc.format.extent 230 p. en_US
dc.format.extent 13916825 bytes
dc.format.extent 13916580 bytes
dc.format.mimetype application/pdf
dc.format.mimetype application/pdf
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.subject Aeronautics and Astronautics en_US
dc.title Blade passage flow structure effects on axial compressor rotating stall inception en_US
dc.type Thesis en_US Ph.D. en_US
dc.contributor.department Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics en_US
dc.identifier.oclc 36266242 en_US

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