Buckling Behavior of FG-CNT Reinforced Composite Conical Shells Subjected to a Combined Loading

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dc.authoridhttps://orcid.org/0000-0002-5968-3382en_US
dc.authoridhttps://orcid.org/0000-0001-7153-4307en_US
dc.contributor.authorSofiyev, Abdullah H.
dc.contributor.authorTornabene, Francesco
dc.contributor.authorDimitri, Rossana
dc.contributor.authorKuruoğlu, Nuri
dc.date.accessioned2020-05-02T00:26:17Z
dc.date.available2020-05-02T00:26:17Z
dc.date.issued2020en_US
dc.departmentMühendislik ve Mimarlık Fakültesien_US
dc.descriptionDocument Information Language:English Accession Number: WOS:000526090400019 PubMed ID: 3212108en_US
dc.description.abstractThe buckling behavior of functionally graded carbon nanotube reinforced composite conical shells (FG-CNTRC-CSs) is here investigated by means of the first order shear deformation theory (FSDT), under a combined axial/lateral or axial/hydrostatic loading condition. Two types of CNTRC-CSs are considered herein, namely, a uniform distribution or a functionally graded (FG) distribution of reinforcement, with a linear variation of the mechanical properties throughout the thickness. The basic equations of the problem are here derived and solved in a closed form, using the Galerkin procedure, to determine the critical combined loading for the selected structure. First, we check for the reliability of the proposed formulation and the accuracy of results with respect to the available literature. It follows a systematic investigation aimed at checking the sensitivity of the structural response to the geometry, the proportional loading parameter, the type of distribution, and volume fraction of CNTs.en_US
dc.identifier.doi10.3390/nano10030419en_US
dc.identifier.issn2079-4991
dc.identifier.issue3en_US
dc.identifier.pmid32121081en_US
dc.identifier.scopus2-s2.0-85081011575en_US
dc.identifier.scopusqualityQ1en_US
dc.identifier.urihttps://hdl.handle.net/11363/2118
dc.identifier.urihttps://doi.org/
dc.identifier.volume10en_US
dc.identifier.wosWOS:000526090400019en_US
dc.identifier.wosqualityQ1en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.indekslendigikaynakPubMeden_US
dc.language.isoenen_US
dc.publisherMDPI, ST ALBAN-ANLAGE 66, CH-4052 BASEL, SWITZERLANDen_US
dc.relation.ispartofNANOMATERIALSen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
dc.subjectnanocompositesen_US
dc.subjectbucklingen_US
dc.subjectFG-CNTRCen_US
dc.subjecttruncated coneen_US
dc.subjectcritical combined loadsen_US
dc.subjectCOMBINED EXTERNAL-PRESSUREen_US
dc.subjectCOMBINED AXIAL-COMPRESSIONen_US
dc.subjectGRADED CYLINDRICAL-SHELLSen_US
dc.subjectRADIAL MECHANICAL LOADSen_US
dc.subjectFREE-VIBRATIONen_US
dc.subjectELASTIC FOUNDATIONSen_US
dc.subjectDEFORMATIONen_US
dc.subjectSTABILITYen_US
dc.subjectPARADIGMen_US
dc.titleBuckling Behavior of FG-CNT Reinforced Composite Conical Shells Subjected to a Combined Loadingen_US
dc.typeArticleen_US

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