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dc.contributor.authorMonge, J
dc.contributor.authorMantari, J
dc.contributor.authorYarasca, J
dc.contributor.authorArciniega, R
dc.date.accessioned2024-12-06T10:44:09Z
dc.date.available2024-12-06T10:44:09Z
dc.date.issued2019-02-26
dc.identifier.doi10.1088/1757-899x/473/1/012006
dc.identifier.urihttp://hdl.handle.net/10757/682630
dc.description.abstractThis study presents a static analysis of laminated composite doubly curved shells using a refined kinematic model with polynomial and non-polynomial functions. In particular Maclaurin, trigonometric, exponential and zig-zag functions are employed. Refined models are based on the Equivalent Single Layer theories and obtained by using Carrera Unified formulation. The shell model is subjected to different mechanical loading such as bi-sinusoidal, uniform and point load. The governing equations are derived from the principle of virtual displacement and solved via Navier-Type closed form solutions. The results are compared with Layer-wise and higher-order shear deformation solutions available in the literature. It is shown that refined models with non-polynomial terms are capable of accurately predicting the through-the-thickness displacements and stress distributions with a low computational effort.es_PE
dc.formatapplication/pdfes_PE
dc.language.isoenges_PE
dc.publisherIOP Publishinges_PE
dc.rightsinfo:eu-repo/semantics/openAccesses_PE
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 International*
dc.rights.urihttp://iopscience.iop.org/info/page/text-and-data-mining
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectHybrid Refined Modelses_PE
dc.subjectLaminated composite doubly curved shellses_PE
dc.subjectRefined kinematic modeles_PE
dc.titleBending Response of Doubly Curved Laminated Composite Shells using Hybrid Refined Modelses_PE
dc.typeinfo:eu-repo/semantics/articlees_PE
dc.identifier.eissn1757-899X
dc.identifier.journalIOP Publishinges_PE
dc.source.journaltitleIOP Conference Series: Materials Science and Engineering
dc.source.volume473
dc.source.beginpage012006
refterms.dateFOA2024-12-06T10:44:10Z
dc.identifier.isni0000 0001 2196 144X


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