A novel versatile multilayer hybrid stress solid-shell element

DOI10.1007/s00466-012-0749-zzbMath1366.74074OpenAlexW1981403292MaRDI QIDQ356802

K. Rah, Joris Degrieck, Wim Van Paepegem

Publication date: 26 July 2013

Published in: Computational Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00466-012-0749-z

zbMATH Keywords

interlaminar stressassumed natural strainsenhanced assumed strainshybrid stress solid-shell elementlocking freemultifield variational principlemultilayer anisotropic composites

Mathematics Subject Classification ID

Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Shells (74K25)

Related Items (1)

A quadrilateral shell element with degree of freedom to represent thickness-stretch

Cites Work

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• A partial hybrid stress solid-shell element for the analysis of laminated composites
• State-of-the-art development of hybrid/mixed finite element method
• Finite elements based on consistently assumed stresses and displacements
• Hybrid-stress isoparametric elements for moderately thick and thin multilayer plates
• Stress fields in composite laminates
• Optimal solid shells for nonlinear analyses of multilayer composites. I: Statics.
• Optimal solid shells for nonlinear analyses of multilayer composites. II: Dynamics.
• Development of a one-point quadrature shell element for nonlinear applications with contact and anisotropy.
• Physical stabilization of the 4-node shell element with one point quadrature
• A theoretical and computational model for isotropic elastoplastic stress analysis in shells at large strains
• A 4-node finite shell element for the implementation of general hyperelastic 3D-elasticity at finite strains
• On the formulation of enhanced strain finite elements in finite deformations
• A reduced integration solid-shell finite element based on the EAS and the ANS concept-Large deformation problems
• On the suppression of zero energy deformation modes
• Rational approach for assumed stress finite elements
• A Simple Higher-Order Theory for Laminated Composite Plates
• A new one-point quadrature enhanced assumed strain (EAS) solid-shell element with multiple integration points along thickness—part II: nonlinear applications
• Partial hybrid stress element for vibrations of thick laminated composite plates
• A reduced integration solid-shell finite element based on the EAS and the ANS concept-Geometrically linear problems
• A large deformation solid-shell concept based on reduced integration with hourglass stabilization
• Enhanced assumed strain (EAS) and assumed natural strain (ANS) methods for one-point quadrature solid-shell elements
• A traction-free-edge hybrid-stress element for the analysis of edge effects in cross-ply laminates
• Hybrid stress reduced-Mindlin elements for thin multilayer plates
• Relations between incompatible displacement model and hybrid stress model
• A three-dimensional hybrid stress isoparametric element for the analysis of laminated composite plates
• Parametrized multifield variational principles in elasticity: I. Mixed functionals
• Parametrized multifield variational principles in elasticity: II. Hybrid functionals and the free formulation
• A rational approach for choosing stress terms for hybrid finite element formulations
• Comparison of hybrid-stress element through-thickness distributions corresponding to a high-order plate theory
• A hybrid-stress finite-element formulation for thick multilayer laminates
• Finite Elements Based Upon Mindlin Plate Theory With Particular Reference to the Four-Node Bilinear Isoparametric Element
• Improvements on the higher order plate element with partial hybrid stress model
• A non-conforming element for stress analysis
• A systematic development of ‘solid-shell’ element formulations for linear and non-linear analyses employing only displacement degrees of freedom
• A three‐dimensional multilayer composite finite element for stress analysis of composite laminates
• Development of shear locking-free shell elements using an enhanced assumed strain formulation
• Classification of stress modes in assumed stress fields of hybrid finite elements
• A geometrical non-linear brick element based on the EAS-method
• A new volumetric and shear locking‐free 3D enhanced strain element
• An assumed strain approach avoiding artificial thickness straining for a non‐linear 4‐node shell element
• Towards efficient and robust elements for 3D-soil plasticity
• A class of mixed assumed strain methods and the method of incompatible modes
• EAS‐elements for two‐dimensional, three‐dimensional, plate and shell structures and their equivalence to HR‐elements
• A new one-point quadrature enhanced assumed strain (EAS) solid-shell element with multiple integration points along thickness: Part I-geometrically linear applications
• A variational justification of the assumed natural strain formulation of finite elements—I. Variational principles
• A variational justification of the assumed natural strain formulation of finite elements—II. The C0 four-node plate element
• ON THE BOUNDS OF EIGENVALUES

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