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

dc.contributor.advisorC.S. Tan.en_US
dc.contributor.authorRenaud, Earl Williamen_US
dc.date.accessioned2008-11-07T18:57:29Z
dc.date.available2008-11-07T18:57:29Z
dc.date.copyright1991en_US
dc.date.issued1991en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/43059
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1991.en_US
dc.descriptionIncludes bibliographical references (leaves 166-170).en_US
dc.description.statementofresponsibilityby Earl William Renaud.en_US
dc.format.extentxiv, 170 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.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.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronauticsen_US
dc.titleSecondary flow, total pressure loss and the effect of circumferential distortions in axial turbine cascadesen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc24400925en_US


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