Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/6393
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dc.contributor.authorSong, Hao.en_US
dc.date.accessioned2008-09-17T11:13:49Z-
dc.date.available2008-09-17T11:13:49Z-
dc.date.copyright2003en_US
dc.date.issued2003-
dc.identifier.urihttp://hdl.handle.net/10356/6393-
dc.description.abstractDelamination buckling is a failure scenario that lessens the structural integrity of laminated composite structural members. In the present work an analytical model is studied for inhomogeneous clamped beams with through-the-width multiple delaminations, located arbitrarily in both the spanwise and thicknesswise directions. The beam is modeled as seven separate component segments, each analyzed as an Euler beam with the "free mode deformation" assumption. Boundary conditions, continuity conditions of the displacement, slope, moment, shear force, and additional axial force compatibility equations are used to generate a system of 37 linear, homogeneous algebraic equations. This system of equations governs the behavior of the delaminated beam when subjected to compressive loading.en_US
dc.rightsNanyang Technological Universityen_US
dc.subjectDRNTU::Engineering::Materials::Composite materials-
dc.titleLaminate composites with multiple delaminationsen_US
dc.typeThesisen_US
dc.contributor.supervisorShu, Dong Weien_US
dc.contributor.schoolSchool of Mechanical and Production Engineeringen_US
dc.description.degreeMaster of Science (Mechanics & Processing of Materials)en_US
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