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dc.contributor.advisorJohn Dugundji.en_US
dc.contributor.authorKim, Taehyoun, 1959-en_US
dc.date.accessioned2008-11-07T19:20:58Z
dc.date.available2008-11-07T19:20:58Z
dc.date.copyright1992en_US
dc.date.issued1992en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/43251
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1992.en_US
dc.descriptionIncludes bibliographical references (leaves 206-211).en_US
dc.description.statementofresponsibilityby Taehyoun Kim.en_US
dc.format.extentxiii, 226 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/1721.1/7582en_US
dc.subjectAeronautics and Astronauticsen_US
dc.titleNonlinear large amplitude structural and aeroelastic behavior of composite rotor blades at large static deflectionen_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc26622965en_US


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