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dc.contributor.advisorH.H. Pian.en_US
dc.contributor.authorLi, Ming-Sangen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2008-02-04T20:51:07Z
dc.date.available2008-02-04T20:51:07Z
dc.date.copyright1989en_US
dc.date.issued1989en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/40145
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.en_US
dc.descriptionIncludes bibliographical references (leaves 259-272).en_US
dc.description.statementofresponsibilityby Ming-Sang Li.en_US
dc.format.extent279 leavesen_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/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.titleHigher order laminated composite plate analysis by hybrid 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.oclc22248778en_US


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