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Effects of asymmetric tip clearance on compressor stability

dc.contributor.advisorEdward M. Greitzer.en_US
dc.contributor.authorGraf, Martin Bowyeren_US
dc.date.accessioned2005-09-26T18:49:42Z
dc.date.available2005-09-26T18:49:42Z
dc.date.copyright1996en_US
dc.date.issued1996en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/28162
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1996.en_US
dc.descriptionIncludes bibliographical references (leaves 52-54).en_US
dc.description.statementofresponsibilityby Martin Bowyer Graf.en_US
dc.format.extent68 leavesen_US
dc.format.extent3061705 bytes
dc.format.extent3068494 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoen_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 Astronauticsen_US
dc.titleEffects of asymmetric tip clearance on compressor stabilityen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc35264034en_US


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