Assessment of 4-node EAS-ANS shell elements for large deformation analysis (Q1015718)

scientific article; zbMATH DE number 5552407

Language	Label	Description	Also known as
English	Assessment of 4-node EAS-ANS shell elements for large deformation analysis	scientific article; zbMATH DE number 5552407

Statements

instance of

scholarly article

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title

Assessment of 4-node EAS-ANS shell elements for large deformation analysis (English)

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author

Boštjan Brank

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published in

Computational Mechanics

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publication date

8 May 2009

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zbMATH Keywords

Reissner-Mindlin theory

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displacement-compatible strains

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transverse shear

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describes a project that uses

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full work available at URL

https://doi.org/10.1007/s00466-007-0233-3

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cites work

EAS‐elements for two‐dimensional, three‐dimensional, plate and shell structures and their equivalence to HR‐elements

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A four-node plate bending element based on Mindlin/Reissner plate theory and a mixed interpolation

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Composite laminates: Nonlinear interlaminar stress analysis by multi-layer shell elements

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A nonlinear extensible 4-node shell element based on continuum theory and assumed strain interpolations

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A 4-node finite shell element for the implementation of general hyperelastic 3D-elasticity at finite strains

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Q4365975

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Q4360602

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On the relation between different parametrizations of finite rotations for shells

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Three‐dimensional extension of non‐linear shell formulation based on the enhanced assumed strain concept

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Finite element concepts for finite elastoplastic strains and isotropic stress response in shells: Theoretical and computational analysis

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Structural analysis of composite laminates using a mixed hybrid shell element

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Stress resultant geometrically exact form of classical shell model and vector‐like parameterization of constrained finite rotations

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Hyperelasticity and physical shear buckling of a block predicted by the Cosserat point element compared with inelasticity and hourglassing predicted by other element formulations

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Shape optimization of truss-stiffened shell structures with variable thickness

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Efficient handling of stability problems in shell optimization by asymmetric ‘worst-case’ shape imperfection

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Automatic generation of finite-element code by simultaneous optimization of expressions

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On `best' shell models -- from classical shells, degenerated and multi-layered concepts to 3D

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An investigation of a finite rotation four node assumed strain shell element

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Families of 4-node and 9-node finite elements for a finite deformation shell theory. An assessment of hybrid stress, hybrid strain and enhanced strain elements

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A class of mixed assumed strain methods and the method of incompatible modes

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Geometrically non-linear enhanced strain mixed methods and the method of incompatible modes

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Optimal solid shells for nonlinear analyses of multilayer composites. I: Statics.

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Optimal solid shells for nonlinear analyses of multilayer composites. II: Dynamics.

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The linearized three-dimensional beam theory of naturally curved and twisted beams: The strain vector formulation

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Identifiers

zbMATH Open document ID

1161.74049

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Mathematics Subject Classification ID

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10.1007/S00466-007-0233-3

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Sitelinks

Mathematics(1 entry)

mardi Publication:1015718