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dc.contributor.advisorÖzütok, Atilla
dc.contributor.authorMadenci, Emrah
dc.date.accessioned2021-01-27T10:47:23Z
dc.date.available2021-01-27T10:47:23Z
dc.date.issued2020-01-10
dc.identifier.issn1225-4568
dc.identifier.urihttp://hdl.handle.net/20.500.12498/5045
dc.description.abstractThis study presents a 4 node, 11 DOF/node plate element based on higher order shear deformation theory for lamina composite plates. The theory accounts for parabolic distribution of the transverse shear strain through the thickness of the plate. Differential field equations of composite plates are obtained from energy methods using virtual work principle. Differential field equations of composite plates are obtained from energy methods using virtual work principle. These equations were transformed into the operator form and then transformed into functions with geometric and dynamic boundary conditions with the help of the Gateaux differential method, after determining that they provide the potential condition. Boundary conditions were determined by performing variational operations. By using the mixed finite element method, plate element named HOPLT44 was developed. After coding in FORTRAN computer program, finite element matrices were transformed into system matrices and various analyzes were performed. The current results are verified with those results obtained in the previous work and the new results are presented in tables and graphs.en_US
dc.language.isoenen_US
dc.publisherSTRUCTURAL ENGINEERING AND MECHANICSen_US
dc.subjectcomposite plateen_US
dc.subjecthigh order shear deformation theoryen_US
dc.subjectfinite element methoden_US
dc.subjectstatic analysisen_US
dc.subjectenergy principleen_US
dc.titleVariational approximate for high order bending analysis of laminated composite platesen_US
dc.typeArticleen_US


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