Composite laminates: Nonlinear interlaminar stress analysis by multi-layer shell elements
From MaRDI portal
Publication:1574317
DOI10.1016/S0045-7825(99)00267-4zbMath0981.74061MaRDI QIDQ1574317
A. Eckstein, Yavuz Başar, Mikhail Itskov
Publication date: 13 November 2000
Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)
parametrizationlinearizationEuler anglesinterlaminar stressesfinite rotationsorthotropic materialsstabilization algorithmenhanced strain formulationassumed strain conceptmulti-director shell theorymulti-layer shell-elementquadratic approximation of displacement fieldthrough-thickness stress distributionupdated rotation formulation
Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30) Shells (74K25)
Related Items (14)
Non-linear exact geometry 12-node solid-shell element with three translational degrees of freedom per node ⋮ Finite element linear and nonlinear, static and dynamic analysis of structural elements, an addendum ⋮ Finite deformation higher-order shell models and rigid-body motions ⋮ Passive and active fiber reorientation in anisotropic materials ⋮ Discrete double directors shell element for the functionally graded material shell structures analysis ⋮ Nonlinear strain--displacement equations exactly representing large rigid-body motions. I: Timoshenko--Mindlin shell theory ⋮ A 4-Node Co-Rotational Quadrilateral Composite Shell Element ⋮ A global-local discontinuous Galerkin shell finite element for small-deformation analysis of multi-layered composites ⋮ A generalized orthotropic hyperelastic material model with application to incompressible shells ⋮ Efficient hybrid-EAS solid element for accurate stress prediction in thick laminated beams, plates, and shells ⋮ Consistent micro-macro transitions at large objective strains in curvilinear convective coordinates ⋮ A general high‐order finite element formulation for shells at large strains and finite rotations ⋮ Assessment of 4-node EAS-ANS shell elements for large deformation analysis ⋮ Nonlinear shell models with seven kinematic parameters
Cites Work
- Unnamed Item
- Unnamed Item
- Unnamed Item
- On a stress resultant geometrically exact shell model. II: The linear theory; computational aspects
- A high-order laminated plate theory with improved in-plane responses
- A consistent theory of geometrically nonlinear shells with an independent rotation vector
- Analysis of free damped vibration of laminated composite plates and shells
- On a stress resultant geometrically exact shell model. IV: Variable thickness shells with through-the-thickness stretching
- Postbuckling analysis of viscoelastic laminated plates using higher-order theory
- 'Best' transverse shearing and stretching shell theory for nonlinear finite element simulations
- Nonlinear analysis of multilayered shells
- Refined shear-deformation models for composite laminates with finite rotations
- On an isoparametric finite-element for composite laminates with finite rotations
- A nonlinear composite shell element with continuous interlaminar shear stresses
- Nonlinear shell formulations for complete three-dimensional constitutive laws including composites and laminates
- Finite element analysis of smooth, folded and multi-shell structures
- A note on enhanced strain methods for large deformations
- Finite-rotation theories for composite laminates
- A theory and finite element formulation of shells at finite deformations involving thickness change: Circumventing the use of a rotation tensor
- Constitutive model and finite element formulation for large strain elasto-plastic analysis of shells
- An excursion into large rotations
- On a stress resultant geometrically exact shell model. VII: Shell intersections with 5/6-DOF finite element formulations
- A 4-node finite shell element for the implementation of general hyperelastic 3D-elasticity at finite strains
- A layered composite shell element for elastic and thermoelastic stress and stability analysis at large deformations
- Analysis of laminated composite plates using a higher-order shear deformation theory
- On the Variational Foundations of Assumed Strain Methods
- A multi‐director formulation for elastic—viscoelastic layered shells
- Analysis of layered composite plates using a high-order deformation theory
- Three‐dimensional extension of non‐linear shell formulation based on the enhanced assumed strain concept
- Triangular finite element for analysis of thick laminated shells
- A refined analysis of laminated plates by finite element displacement methods—I. Fundamentals and static analysis
- 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
- On refined computational models of composite laminates
- A plate bending element based on a generalized laminate plate theory
This page was built for publication: Composite laminates: Nonlinear interlaminar stress analysis by multi-layer shell elements
