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dc.contributor.advisorJames H. Williams, Jr.en_US
dc.contributor.authorUrrutia Valenzuela, Robertoen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Mechanical Engineering.en_US
dc.date.accessioned2011-03-24T20:27:21Z
dc.date.available2011-03-24T20:27:21Z
dc.date.copyright2010en_US
dc.date.issued2010en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/61923
dc.descriptionThesis (S.M. in Naval Architecture and Marine Engineering )--Massachusetts Institute of Technology, Dept. of Mechanical Engineering; and, Thesis (S.M. in Mechanical Engineering)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2010.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (p. 71-73).en_US
dc.description.abstractGlass fiber / vinyl ester composite laminates represent an important class of modem fiber composites being proposed or used in state-of-the-art shipbuilding. This thesis examined the effectiveness of chopped strand mat (CSM) plug repairs of glass fiber / vinyl ester woven roving laminates subjected to in-plane shear and bending. An advantage of this type of repair scheme is its simplicity when compared to more traditional schemes such as scarf or step repairs. The stress concentrations around circular holes in glass fiber / vinyl ester woven roving laminates subjected to in-plane shear and bending were calculated before and after repairs using CSM plugs, also of glass fiber / vinyl ester, having varying fiber volume fractions. The laminates were orthotropic and ranged from balanced to unidirectional woven roving, and the CSM plug fiber volume fractions ranged from 0 to 0.40. For in-plane shear stress, as the plug fiber volume fraction increased from 0 to 0.40, the maximum stress concentration along the circular holes in the laminate was reduced from about 25% to 61%. For in-plane bending, as the plug fiber volume fraction increased from 0 to 0.40, the maximum stress concentration in the laminate was reduced from about 25% to 45%.en_US
dc.description.statementofresponsibilityby Roberto Urrutia Valenzuela.en_US
dc.format.extent79 p.en_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.subjectMechanical Engineering.en_US
dc.titlePlug repairs of marine glass fiber / vinyl ester laminates subjected to in-plane shear stress or in-plane bending momenten_US
dc.typeThesisen_US
dc.description.degreeS.M.in Mechanical Engineeringen_US
dc.description.degreeS.M.in Naval Architecture and Marine Engineeringen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Mechanical Engineering
dc.identifier.oclc707327853en_US


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