A crack tip tracking algorithm for cohesive interface element analysis of fatigue delamination propagation in composite materials

INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES

卷:49

Article

Kawashita, Luiz F.¹  Hallett, Stephen R.¹ 

[1] Univ Bristol, ACCIS, Bristol BS8 1TR, Avon, England

关键词: Cohesive;    Element;    Fatigue;    Delamination;    Fibre;    Composite;   

DOI  :  10.1016/j.ijsolstr.2012.03.034

来源: Elsevier

【 摘 要 】

A novel approach is proposed for the use of cohesive elements in the analysis of delamination propagation in composite materials under high-cycle fatigue loading. The method is applicable to delamination propagation within the Paris-law regime and is suitable for the analysis of three-dimensional structures typical of aerospace applications. The major advantages of the proposed formulation are its complete independence of the cohesive zone length - which is a geometry-dependent parameter - and its relative insensitivity to mesh refinement. This is only possible via the introduction of three nonlocal algorithms, which provide (i) automated three-dimensional tracking of delamination fronts, (ii) an estimation of direction of crack propagation and (iii) accurate and mesh-insensitive integration of strain energy release rate. All calculations are updated at every increment of an explicit time-integration finite element solution, which models the envelopes of forces and displacements with an assumption of underlying constant cyclic loading. The method was implemented as a user-defined subroutine in the commercial finite element software LS-Dyna and supports the analysis of complex three-dimensional models. Results are presented for benchmark cases such as specimens with central cut plies and centrally-loaded circular plates. Accurate predictions of delamination growth rates are observed for different mesh topologies in agreement with the Paris-laws of the material. (C) 2012 Elsevier Ltd. All rights reserved.

【 授权许可】

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