A nine-node assumed strain finite element for large-deformation analysis of laminated shells

DOI<777::AID-NME365>3.0.CO;2-P 10.1002/(SICI)1097-0207(19980715)42:5<777::AID-NME365>3.0.CO;2-PzbMath0915.73059OpenAlexW2082615981MaRDI QIDQ4219960

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Publication date: 11 November 1998

Full work available at URL: https://doi.org/10.1002/(sici)1097-0207(19980715)42:5<777::aid-nme365>3.0.co;2-p

zbMATH Keywords

element-based Lagrangian formulationarc-length control methodequivalent natural constitutive equationmulti-layer effectsuccessive finite rotations

Mathematics Subject Classification ID

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

Related Items (5)

Free and forced vibration analysis of laminated composite plates and shells using a 9-node assumed strain shell element ⋮ Large elastic deformation of micromorphic shells. Part II. Isogeometric analysis ⋮ BUCKLING OF SYMMETRICALLY LAMINATED COMPOSITE PLATES USING THE ELEMENT-FREE GALERKIN METHOD ⋮ Geometrically Exact Nonlinear Extended-Reissner/Mindlin Shells: Fundamentals, Finite Element Formulation, Elasticity ⋮ Finite element linear and nonlinear, static and dynamic analysis of structural elements – an addendum – A bibliography (1996‐1999)

Cites Work

• Flexural analysis of laminated composites using refined higher-order \(C^ o\) plate bending elements
• On the bootstrap of the sample mean in the infinite variance case
• Triangular finite element for analysis of thick laminated plates

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