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dc.contributor.advisorPaul A. Lagace.en_US
dc.contributor.authorBrewer, John Cen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2009-06-30T16:03:06Z
dc.date.available2009-06-30T16:03:06Z
dc.date.copyright1985en_US
dc.date.issued1985en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/45686
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1985.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.en_US
dc.descriptionIncludes bibliographical references.en_US
dc.description.statementofresponsibilityby John Charles Brewer.en_US
dc.format.extent184 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 free edge delamination of graphite/epoxy laminatesen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc13195277en_US


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