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dc.contributor.advisorEdward M. Greitzer.en_US
dc.contributor.authorCho, Donald L. (Donald Lee)en_US
dc.date.accessioned2009-10-01T15:06:35Z
dc.date.available2009-10-01T15:06:35Z
dc.date.copyright1995en_US
dc.date.issued1995en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/47391
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.en_US
dc.descriptionIncludes bibliographical references (p. 89-90).en_US
dc.description.statementofresponsibilityby Donald L. Cho.en_US
dc.format.extent90 p.en_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.titleEffect of vortex core stagnation pressure on tip clearance flow blockage in turbomachinesen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc34314610en_US


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