Hybrid strain based geometrically nonlinear laminated composite triangular shell finite elements

DOI10.1016/S0168-874X(99)00028-1zbMath0954.74074OpenAlexW2090939627MaRDI QIDQ1960546

Yanyan Li

Publication date: 12 January 2000

Published in: Finite Elements in Analysis and Design (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0168-874x(99)00028-1

zbMATH Keywords

finite strainlarge deformationgeometrically nonlinear analysisupdated Lagrangian formulationHellinger-Reissner variational principlefinite rotationfirst-order lamination theoryflat triangular shell finite elementsincremental second Piola-Kirchhoff stressincremental Washizu strainlarge-scale laminated compositepseudo-load vectorthinning effect

Mathematics Subject Classification ID

Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Membranes (74K15)

Related Items (6)

Finite element linear and nonlinear, static and dynamic analysis of structural elements, an addendum ⋮ Nonlinear strain--displacement equations exactly representing large rigid-body motions. I: Timoshenko--Mindlin shell theory ⋮ A simple displacement-based 3-node triangular element for linear and geometrically nonlinear analysis of laminated composite plates ⋮ Finite element linear and nonlinear, static and dynamic analysis of structural elements – an addendum – A bibliography (1996‐1999) ⋮ A 6-node co-rotational triangular elasto-plastic shell element ⋮ A stabilized co-rotational curved quadrilateral composite shell element

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