A stabilized hybrid-stress solid element for geometrically nonlinear homogeneous and laminated shell analyses
From MaRDI portal
Publication:1348318
DOI10.1016/S0045-7825(01)00362-0zbMath1098.74714OpenAlexW1980984619MaRDI QIDQ1348318
Publication date: 15 May 2002
Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/s0045-7825(01)00362-0
Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Shells (74K25)
Related Items
A seven-parameter spectral/\(hp\) finite element formulation for isotropic, laminated composite and functionally graded shell structures, Application of the continuum shell finite element SHB8PS to sheet forming simulation using an extended large strain anisotropic elastic-plastic formulation, An efficient solid shell material point method for large deformation of thin structures, A co-rotational triangular finite element for large deformation analysis of smooth, folded and multi-shells, On a physically stabilized one point finite element formulation for three-dimensional finite elasto-plasticity, Geometrically Exact Nonlinear Extended-Reissner/Mindlin Shells: Fundamentals, Finite Element Formulation, Elasticity
Uses Software
Cites Work
- Unnamed Item
- Finite elements based on consistently assumed stresses and displacements
- Large deflection and post-buckling analysis of shell structures
- On a stress resultant geometrically exact shell model. III: Computational aspects of the nonlinear theory
- An explicit hybrid-stabilized 9-node Lagrangian shell element
- 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
- A 4-node finite shell element for the implementation of general hyperelastic 3D-elasticity at finite strains
- A nine-node assumed-strain finite element for composite plates and shells
- An eighteen-node solid element for thin shell analysis
- A solid element formulation for large deflection analysis of composite shell structures
- Assumed strain stabilization procedure for the 9‐node Lagrange shell element
- Hybrid semiLoof element for buckling of thin-walled structures
- A uniform strain hexahedron and quadrilateral with orthogonal hourglass control
- A fast incremental/iterative solution procedure that handles “snap-through”
- A finite rotation shell theory with application to composite structures
- A systematic development of ‘solid-shell’ element formulations for linear and non-linear analyses employing only displacement degrees of freedom
- A novel approach for devising higher‐order hybrid elements
- A hybrid stress ANS solid-shell element and its generalization for smart structure modelling. Part I?solid-shell element formulation
- A continuum‐based shell theory for non‐linear applications
- An assumed strain approach avoiding artificial thickness straining for a non‐linear 4‐node shell element
- An efficient assumed strain element model with six DOF per node for geometrically non‐linear shells
- Hybrid hexahedral element for solids, plates, shells and beams by selective scaling