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dc.contributor.advisorAlan Harry Epstein.en_US
dc.contributor.authorPreiser, Uriel Zen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-08-05T18:34:21Z
dc.date.available2005-08-05T18:34:21Z
dc.date.copyright1983en_US
dc.date.issued1984en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/15593
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby Uriel Z. Preiser.en_US
dc.format.extent151 leavesen_US
dc.format.extent8502316 bytes
dc.format.extent8502075 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.titleStagger angle effects on impingement cooling of a rotating turbine bladeen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc11905608en_US


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