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dc.contributor.advisorJames E. McCune.en_US
dc.contributor.authorDang, Thong Quocen_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2018-12-18T20:04:21Z
dc.date.available2018-12-18T20:04:21Z
dc.date.copyright1983en_US
dc.date.issued1983en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/119780
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1983.en_US
dc.descriptionMicrofiche copy available in Archives and Barkeren_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby Thong Quoc Dang.en_US
dc.format.extent125 leavesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleA two-dimensional design method for highly-loaded blades 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.oclc11137090en_US


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