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dc.contributor.advisorJames W. Mar.en_US
dc.contributor.authorNolet, Stephen Cen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2010-01-07T20:21:18Z
dc.date.available2010-01-07T20:21:18Z
dc.date.copyright1984en_US
dc.date.issued1984en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/50277
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1984.en_US
dc.descriptionMicrofiche copy available in Archives and Barker.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby Stephen C. Nolet.en_US
dc.format.extent181 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 Astronautics.en_US
dc.titleThe effect of ply thickness on the initiation and growth of delamination in graphite/epoxy laminates with holes under compressive cyclic loadingen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc12264853en_US


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