dc.creatorMantari, J.L
dc.creatorRamos, I.A
dc.creatorMonge, J.C.
dc.date.accessioned2021-03-16T23:23:01Z
dc.date.available2021-03-16T23:23:01Z
dc.date.created2021-03-16T23:23:01Z
dc.date.issued2019-04
dc.identifier1000-9361
dc.identifierhttps://hdl.handle.net/20.500.12815/198
dc.identifierhttps://doi.org/10.1016/j.cja.2019.02.001
dc.identifierChinese Journal of Aeronautics
dc.description.abstractThe mechanical behavior of advanced composites can be modeled mathematically through unknown variables and Shear Strain Thickness Functions (SSTFs). Such SSTFs can be of polynomial or non-polynomial nature and some parameters of non-polynomial SSTFs can be optimized to get optimal results. In this paper, these parameters are called “r” and “s” and they are the argument of the trigonometric SSTFs introduced within the Carrera Unified Formulation (CUF). The Equivalent Single Layer (ESL) governing equations are obtained by employing the Principle of Virtual Displacement (PVD) and are solved using Navier method solution. Furthermore, trigonometric expansion with Murakami theory was implemented in order to reproduce the Zig-Zag effects which are important for multilayer structures. Several combinations of optimization parameters are evaluated and selected by different criteria of average error. Results of the present unified trigonometrical theory with CUF bases confirm that it is possible to improve the stress and displacement results through the thickness distribution of models with reduced unknown variables. Since the idea is to find a theory with reduced numbers of unknowns, the present method appears to be an appropriate technique to select a simple model. However these optimization parameters depend on the plate geometry and the order of expansion or unknown variables. So, the topic deserves further research.
dc.languageeng
dc.publisherElsevier
dc.rightshttp://creativecommons.org/licenses/by-nc-nd/4.0/
dc.rightsinfo:eu-repo/semantics/openAccess
dc.sourceRepositorio Institucional UTEC
dc.sourceUniversidad de Ingeniería y Tecnología - UTEC
dc.subjectComposite materials
dc.subjectPlates (structural components)
dc.subjectPlating
dc.subjectShear deformation
dc.subjectShear strain
dc.subjectCarrera unified formulations
dc.subjectEquivalent single layers
dc.subjectPrinciple of virtual displacements
dc.subjectShear deformation theory
dc.subjectStress and displacements
dc.subjectThickness distributions
dc.subjectTrigonometric functions
dc.subjectZig-zag effects
dc.subjectPolynomials
dc.titleNon-polynomial Zig-Zag and ESL shear deformation theory to study advanced composites
dc.typeinfo:eu-repo/semantics/article


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