International Journal of Computational Engineering ScienceVol. 02, No. 01, pp. 137-180 (2001) No AccessA THREE-DIMENSIONAL LAMINATED PLATE FINITE ELEMENT WITH HIGH-ORDER ZIG-ZAG SUBLAMINATE APPROXIMATIONSY. C. YIP and R. C. AVERILLY. C. YIPEngineering & Development Centre, Singapore Technologies Aerospace Ltd., 540 Airport Road, Paya Lebar, Singapore 539938, Singapore Search for more papers by this author and R. C. AVERILLDepartment of Materials Science and Mechanics, Michigan State University, East Lansing, MI 48824-1226, USA Search for more papers by this author https://doi.org/10.1142/S1465876301000271Cited by:8 Previous AboutSectionsPDF/EPUB ToolsAdd to favoritesDownload CitationsTrack CitationsRecommend to Library ShareShare onFacebookTwitterLinked InRedditEmail AbstractThis paper describes a new laminated composite plate theory and associated finite element model that allow variable through-the-thickness refinement, as needed, to capture higher-order thickness effects and interlaminar stresses in laminated composite and sandwich panels. The theory and finite element model utilize a new zig-zag sublaminate concept, in which each computational layer (or sublaminate) contains several, even many, physical layers. Within each sublaminate, a high-order zig-zag kinematic assumption is employed, providing very high accuracy, even when the entire laminate is modeled using only a single sublaminate. The accuracy and efficienty of the model are thus adaptable, depending upon the number of sublaminates used. In order to facilitate through-the-thickness refinement, the finite element model is cast in the form of an eight-noded brick-type element, with displacements and rotations as nodal degrees-of-freedom. At interlaminar element boundaries, interlaminar shear traction degrees-of-freedom are also present, so that transverse shear stress continuity can be enforced through the entire thickness of the laminate, irrespective of the thickness discretization chosen. Numerical examples are presented to demonstrate the effectiveness of the current model for the analysis of laminated composite and sandwich panels that are very thick or thin.Keywords:laminatecompositezig-zagsublaminatefinite elementplate theory FiguresReferencesRelatedDetailsCited By 8Bending analysis of composite laminated and sandwich structures using sublaminate variable-kinematic Ritz modelsM. D’Ottavio, L. Dozio, R. Vescovini and O. Polit1 Nov 2016 | Composite Structures, Vol. 155Multilayered Plate Model with “Adaptive” Representation of Displacements and Temperature Across the Thickness and Fixed D.O.F.Ugo Icardi1 Sep 2011 | Journal of Thermal Stresses, Vol. 34, No. 9Multilayered shell model with variable representation of displacements across the thicknessU. Icardi and L. Ferrero1 Jan 2011 | Composites Part B: Engineering, Vol. 42, No. 1Layerwise zig-zag model with selective refinement across the thicknessU. Icardi and L. Ferrero26 October 2010 | International Journal for Numerical Methods in Engineering, Vol. 84, No. 9Layerwise mixed element with sublaminates approximation and 3D zig-zag field, for analysis of local effects in laminated and sandwich compositesU. Icardi6 September 2006 | International Journal for Numerical Methods in Engineering, Vol. 70, No. 1plate element for global/local analysis of multilayered composites, based on a 3D zig-zag model and strain energy updatingU. Icardi1 Oct 2005 | International Journal of Mechanical Sciences, Vol. 47, No. 10Applications of Zig-Zag Theories to Sandwich BeamsU. Icardi1 Jan 2003 | Mechanics of Advanced Materials and Structures, Vol. 10, No. 1Finite element linear and nonlinear, static and dynamic analysis of structural elements, an addendumJaroslav Mackerle1 Aug 2002 | Engineering Computations, Vol. 19, No. 5 Recommended Vol. 02, No. 01 Metrics History Keywordslaminatecompositezig-zagsublaminatefinite elementplate theoryPDF download
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