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Secondary flow, total pressure loss and the effect of circumferential distortions in axial turbine cascades

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dc.contributor.advisor C.S. Tan. en_US
dc.contributor.author Renaud, Earl William en_US
dc.date.accessioned 2008-11-07T18:57:29Z
dc.date.available 2008-11-07T18:57:29Z
dc.date.copyright 1991 en_US
dc.date.issued 1991 en_US
dc.identifier.uri http://hdl.handle.net/1721.1/43059
dc.description Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991. en_US
dc.description Includes bibliographical references (leaves 166-170). en_US
dc.description.statementofresponsibility by Earl William Renaud. en_US
dc.format.extent xiv, 170 leaves 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 Secondary flow, total pressure loss and the effect of circumferential distortions in axial turbine cascades en_US
dc.type Thesis en_US
dc.description.degree Ph.D. en_US
dc.contributor.department Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics en_US
dc.identifier.oclc 24400925 en_US


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