Failure optimization of geometrically linear/nonlinear laminated composite structures using a two-step hierarchical model adaptivity

DOI10.1016/j.cma.2009.02.033zbMath1229.74115OpenAlexW1965368773MaRDI QIDQ658262

Erik Lund, Josva Kleist, Leon S. Johansen

Publication date: 11 January 2012

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.cma.2009.02.033

zbMATH Keywords

failuremesh refinementgeometrically nonlinear3D composite laminate optimization

Mathematics Subject Classification ID

Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Fracture and damage (74R99) Optimization of other properties in solid mechanics (74P10)

Related Items (4)

Global laminate optimization on geometrically partitioned shell structures ⋮ Optimization formulations for the maximum nonlinear buckling load of composite structures ⋮ Nonlinear buckling optimization of composite structures considering ``worst shape imperfections ⋮ Nonlinear buckling optimization of composite structures

Cites Work

• Unnamed Item
• A Mindlin element for thick and deep shells
• Parametrization in laminate design for optimal compliance
• Adaptive \(hpq\)-finite element methods of hierarchical models for plate- and shell-like structures
• Optimization of multilaminated structures using higher-order deformation models
• Optimal solid shells for nonlinear analyses of multilayer composites. I: Statics.
• Optimal solid shells for nonlinear analyses of multilayer composites. II: Dynamics.
• On `best' shell models -- from classical shells, degenerated and multi-layered concepts to 3D
• A priori modeling error estimates of hierarchical models for elasticity problems for plate- and shell-like structures
• A 4-node finite shell element for the implementation of general hyperelastic 3D-elasticity at finite strains
• A Simple Higher-Order Theory for Laminated Composite Plates
• Sensitivity analysis and optimal design of thin laminated composite structures
• A systematic development of ‘solid-shell’ element formulations for linear and non-linear analyses employing only displacement degrees of freedom
• Buckling sensitivity analysis and optimal design of thin laminated structures
• A hybrid stress ANS solid-shell element and its generalization for smart structure modelling. Part I?solid-shell element formulation
• Mixed-dimensional coupling in finite element models
• An assumed strain approach avoiding artificial thickness straining for a non‐linear 4‐node shell element
• A class of mixed assumed strain methods and the method of incompatible modes

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