Nonlinear forced response of doubly-curved laminated panels composed of cnt patterned layers within first order shear deformation theory

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dc.contributor.authorSofiyev A.H.
dc.date.accessioned2023-11-13T12:10:08Z
dc.date.available2023-11-13T12:10:08Z
dc.date.issued2023en_US
dc.departmentFakülteler, İnsan ve Toplum Bilimleri Fakültesi, Matematik Bölümüen_US
dc.description.abstractIn this study, the solution of the nonlinear forced vibration (NFV) problem of double curvature panels consisting of inhomogeneous (INH) nanocomposite (NC) layers is discussed within first order shear deformation theory (FSDT), taking into account the viscous damping effect. First, the mechanical properties of laminated double curvature panels composed of carbon nanotube patterned layers are modeled mathematically. Then, based on FSDT with a von K´ arman-type ´ nonlinearity derived the nonlinear basic relationships and partial differential equations (PDEs). The expression for the NFV frequency of multilayer panels made of inhomogeneous nano composite layers (INHNCLs) is obtained within FSDT, using the multi-scale method to the nonlinear PDEs for the first time. Finally, the influences of the external excitation, nonlinearity, transverse shear strains, number and arrangement of layers and CNT-models on the forced vibration frequencies are studied in detail.en_US
dc.identifier.doi10.1016/j.tws.2023.111227en_US
dc.identifier.scopus2-s2.0-85173148423en_US
dc.identifier.scopusqualityN/Aen_US
dc.identifier.urihttps://hdl.handle.net/11467/7026
dc.identifier.urihttps://doi.org/10.1016/j.tws.2023.111227
dc.identifier.volume193en_US
dc.identifier.wosWOS:001088848500001en_US
dc.identifier.wosqualityQ1en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.relation.ispartofThin-Walled Structuresen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/embargoedAccessen_US
dc.subjectNonlinear forced vibration, CNT patterned layers, Laminated nanocomposite panels, Multi-scales method, External excitation, Viscous dampingen_US
dc.titleNonlinear forced response of doubly-curved laminated panels composed of cnt patterned layers within first order shear deformation theoryen_US
dc.typeArticleen_US

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