Buckling Characteristics of FGM Plates Subjected to Linearly Varying In-Plane Loads

dc.authorscopusid23013208000
dc.contributor.authorUymaz, Bahar
dc.date.accessioned2022-05-11T14:03:08Z
dc.date.available2022-05-11T14:03:08Z
dc.date.issued2021
dc.departmentFakülteler, Çorlu Mühendislik Fakültesi, Makine Mühendisliği Bölümü
dc.description.abstractThe critical buckling load for a FGM plate under a linearly distributed in-plane load is determined. Material properties of the plate vary exponentially across its thickness. The Ritz method is used to solve the equations formed according to the 3D linear elasticity theory. The effects of different material compositions and dimensions of the plate on its critical buckling load and mode shapes are investigated for three different boundary conditions. © 2021, Springer Science+Business Media, LLC, part of Springer Nature.
dc.identifier.doi10.1007/s11029-021-09934-5
dc.identifier.endpage80
dc.identifier.issn0191-5665
dc.identifier.issue1en_US
dc.identifier.scopus2-s2.0-85102564897
dc.identifier.scopusqualityQ2
dc.identifier.startpage69
dc.identifier.urihttps://doi.org/10.1007/s11029-021-09934-5
dc.identifier.urihttps://hdl.handle.net/20.500.11776/4615
dc.identifier.volume57
dc.identifier.wosWOS:000629864500001
dc.identifier.wosqualityQ4
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.institutionauthorUymaz, Bahar
dc.language.isoen
dc.publisherSpringer
dc.relation.ispartofMechanics of Composite Materials
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectaxial buckling
dc.subjectFGM plate
dc.subjectlinearly varying load
dc.subjectRitz method
dc.subjectCeramic materials
dc.subjectMechanics
dc.subjectCritical buckling loads
dc.subjectDifferent boundary condition
dc.subjectIn-plane loads
dc.subjectLinear elasticity theory
dc.subjectLinearly varying in-plane load
dc.subjectMaterial compositions
dc.subjectMode shapes
dc.subjectRitz methods
dc.subjectBuckling
dc.titleBuckling Characteristics of FGM Plates Subjected to Linearly Varying In-Plane Loads
dc.typeArticle

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