Publication:
The Stability of a Thin Three-Layered Composite Truncated Conical Shell Containing an FGM Layer Subjected to Non-Uniform Lateral Pressure

dc.authorscopusid6603803044
dc.authorscopusid6508376791
dc.authorscopusid13606601000
dc.contributor.authorSofiyev, A.H.
dc.contributor.authorZerin, Z.
dc.contributor.authorKorkmaz, A.
dc.date.accessioned2020-06-21T15:13:06Z
dc.date.available2020-06-21T15:13:06Z
dc.date.issued2008
dc.departmentOndokuz Mayıs Üniversitesien_US
dc.department-temp[Sofiyev] A. Heydaroglu, Department of Civil Engineering, Süleyman Demirel Üniversitesi, Isparta, Isparta, Turkey; [Zerin] Zihni, Department of Civil Engineering, Ondokuz Mayis Üniversitesi, Samsun, Turkey; [Korkmaz] Kasim Armaǧan, Department of Civil Engineering, Süleyman Demirel Üniversitesi, Isparta, Isparta, Turkeyen_US
dc.description.abstractThis paper examines the stability of thin three-layered truncated conical shells containing a functionally graded (FG) layer subjected to non-uniform lateral pressure varying with the longitudinal coordinate. The material properties of the functionally graded layer are assumed to vary continuously through the thickness of the shell, and the variation of properties follows an arbitrary distribution in terms of the volume fractions of the constituents. Further, the fundamental relations for stability and compatibility equations of three-layered truncated conical shells containing an FGM layer have been obtained. These equations, ascertained via Galerkin's method, have been transformed into a pair of time-dependent differential equations. Then, critical non-uniform lateral pressure has been conclusively obtained. This paper is the result of a detailed parametric study conducted to determine the influences of thickness variations in the FG layer, radius-to-thickness ratio, lengths-to-radius ratio, and the material composition and material profile index on the critical parameters of three-layered, truncated, conical shells. Finally, the results will be validated through the comparison of obtained values with those in the existing literature. © 2007.en_US
dc.identifier.doi10.1016/j.compstruct.2007.10.022
dc.identifier.endpage115en_US
dc.identifier.isbn9780080548098
dc.identifier.issn0263-8223
dc.identifier.issue2en_US
dc.identifier.scopus2-s2.0-42649110364
dc.identifier.scopusqualityQ1
dc.identifier.startpage105en_US
dc.identifier.urihttps://doi.org/10.1016/j.compstruct.2007.10.022
dc.identifier.volume85en_US
dc.identifier.wosWOS:000256678200002
dc.identifier.wosqualityQ1
dc.language.isoenen_US
dc.publisherElsevier Sci Ltden_US
dc.relation.ispartofComposite Structuresen_US
dc.relation.journalComposite Structuresen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectCritical Loaden_US
dc.subjectFG Layeren_US
dc.subjectNon-Uniform Lateral Pressureen_US
dc.subjectStabilityen_US
dc.subjectThree-Layered Truncated Conical Shellen_US
dc.titleThe Stability of a Thin Three-Layered Composite Truncated Conical Shell Containing an FGM Layer Subjected to Non-Uniform Lateral Pressureen_US
dc.typeArticleen_US
dspace.entity.typePublication

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