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dc.contributor.advisorBelgacem Jery.en_US
dc.contributor.authorGauthier, Robert P. (Robert Paul), 1965-en_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-08-10T20:06:19Z
dc.date.available2005-08-10T20:06:19Z
dc.date.copyright1990en_US
dc.date.issued1990en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/14150
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1990.en_US
dc.descriptionIncludes bibliographical references (leaf 62).en_US
dc.description.statementofresponsibilityby Robert P. Gauthier.en_US
dc.format.extent99 leavesen_US
dc.format.extent2581744 bytes
dc.format.extent2581503 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
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/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.titleAn investigation of flow field perturbation caused by constant blade tip clearance in a turbineen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc23943733en_US


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