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dc.contributor.advisorTheodore H.H. Pian.en_US
dc.contributor.authorKang, David Sung-Sooen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-08-08T16:30:32Z
dc.date.available2005-08-08T16:30:32Z
dc.date.copyright1986en_US
dc.date.issued1986en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/14973
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1986.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AEROen_US
dc.descriptionBibliography: leaves 257-264.en_US
dc.description.statementofresponsibilityby David Sung-Soo Kang.en_US
dc.format.extent294 leavesen_US
dc.format.extent10444042 bytes
dc.format.extent10443800 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.titleHybrid stress finite element methoden_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc15002351en_US


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