On the solution of thermal buckling problem of moderately thick laminated conical shells containing carbon nanotube originating layers

dc.contributor.authorAvey, Mahmure
dc.contributor.authorFantuzzi, Nicholas
dc.contributor.authorSofiyev, Abdullah
dc.date.accessioned2023-01-30T11:51:39Z
dc.date.available2023-01-30T11:51:39Z
dc.date.issued2022en_US
dc.departmentRektörlük, Bilişim Teknolojileri Uygulama ve Araştırma Merkezien_US
dc.description.abstractThis study presents the solution for the thermal buckling problem of moderately thick laminated conical shells consisting of carbon nanotube (CNT) originating layers. It is assumed that the laminated truncated-conical shell is subjected to uniform temperature rise. The Donnell-type shell theory is used to derive the governing equations, and the Galerkin method is used to find the expression for the buckling temperature in the framework of shear deformation theories (STs). Different transverse shear stress functions, such as the parabolic transverse shear stress (Par-TSS), cosine-hyperbolic shear stress (Cos-Hyp-TSS), and uniform shear stress (U-TSS) functions are used in the analysis part. After validation of the formulation with respect to the existing literature, several parametric studies are carried out to investigate the influences of CNT patterns, number and arrangement of the layers on the uniform buckling temperature (UBT) using various transverse shear stress functions, and classical shell theory (CT).en_US
dc.identifier.doi10.3390/ma15217427en_US
dc.identifier.scopus2-s2.0-85141825151en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.urihttps://hdl.handle.net/11467/6168
dc.identifier.urihttps://doi.org/10.3390/ma15217427
dc.identifier.wosWOS:000882149000001en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.indekslendigikaynakPubMeden_US
dc.language.isoenen_US
dc.publisherMDPIen_US
dc.relation.ispartofMaterialsen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectCNT; nanocomposites; laminated truncated conical shell; thermal buckling; transverse shear stress functions; partial differential equationsen_US
dc.titleOn the solution of thermal buckling problem of moderately thick laminated conical shells containing carbon nanotube originating layersen_US
dc.typeArticleen_US

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