## Abstract The finite element analysis of delamination in laminated composites is addressed using interface elements and an interface damage law. The principles of linear elastic fracture mechanics are indirectly used by equating, in the case of singleβmode delamination, the area underneath the tr
Rotational interface formulation for delamination analysis of composite laminates
β Scribed by N.E. Jansson; R. Larsson
- Publisher
- Elsevier Science
- Year
- 2003
- Tongue
- English
- Weight
- 420 KB
- Volume
- 81
- Category
- Article
- ISSN
- 0045-7949
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β¦ Synopsis
In this paper, delamination progression in a composite laminate is modelled by interface elements within a geometrically non-linear FE analysis setting. With the assumption of small continuum deformations, a rotational interface formulation is obtained from a recently proposed formulation based on the concept of a regularised strong discontinuity, cf. [Int. J. Numer. Meth. Eng. 54 (2002) 473]. The degradation of the stress vector in the cohesive zone is described by a damage-plasticity coupling, which is calibrated analytically against experimental data of mixed-mode fracture energies. The paper is concluded by a couple of numerical examples that describe the predictive capabilities of the interface formulation.
π SIMILAR VOLUMES
This paper concerns with the transient response of composite laminates with multiple delaminations subjected to low-velocity impact by a rigid ball. The "nite element method based on the Mindlin plate theory is employed to describe the motion and deformation of the laminates. A Hertzian-type indenta
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