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dc.contributor.advisorAlan H. Epstein.en_US
dc.contributor.authorShang, Tonghuoen_US
dc.date.accessioned2009-10-01T15:03:23Z
dc.date.available2009-10-01T15:03:23Z
dc.date.copyright1995en_US
dc.date.issued1995en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/47370
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.en_US
dc.descriptionIncludes bibliographical references (p. 195-198).en_US
dc.description.statementofresponsibilityby Tonghuo Shang.en_US
dc.format.extent224 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.titleInfluence of inlet temperature distortion on turbine heat transferen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc32517770en_US


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