Modeling delamination in composite laminates using XFEM by new orthotropic enrichment functions

被引:13
|
作者
Ashari, S. Esna [1 ]
Mohammadi, S. [1 ]
机构
[1] Univ Tehran, Sch Civil Engn, Tehran, Iran
关键词
FINITE-ELEMENT; CRACK-GROWTH; MEDIA;
D O I
10.1088/1757-899X/10/1/012240
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this research, the extended finite element method (XFEM) is improved for modeling interfacial cracks between two orthotropic media by new set of orthotropic enrichment functions. New set of bimaterial orthotropic enrichment functions are developed and utilized in XFEM analysis of linear elastic fracture mechanics of layered composites. Interlaminar crack-tip enrichment functions are derived from analytical asymptotic displacement fields around a traction free interfacial crack. In this procedure, elements containing a crack tip or strong/weak discontinuities are not required to conform to those geometries. The domain interaction integral approach is also adopted in order to numerically evaluate the mixed-mode stress intensity factors. A number of benchmark tests are simulated to assess the performance of the proposed approach and the results are compared to available reference results.
引用
收藏
页数:8
相关论文
共 50 条
  • [41] Dynamic analysis of composite laminates with multiple delamination using improved layerwise theory
    Kim, HS
    Chattopadhyay, A
    Ghoshal, A
    AIAA JOURNAL, 2003, 41 (09) : 1771 - 1779
  • [42] Imaging delamination in composite laminates using perturbation to steady-state wavefields
    Xu, Wei
    Cao, Maosen
    Su, Zhongqing
    Xu, Hao
    Radzienski, Maciej
    Ostachowicz, Wieslaw
    SMART MATERIALS AND STRUCTURES, 2021, 30 (07)
  • [43] Delamination detection in composite laminates using improved surrogate-assisted optimization
    Tong, Huawei
    Pan, Jingwen
    Singh, Hemant Kumar
    Luo, Weili
    Zhang, Zhifang
    Hui, David
    COMPOSITE STRUCTURES, 2021, 277
  • [44] Mode separation of energy release rate for delamination in composite laminates using sublaminates
    Zou, Z
    Reid, SR
    Soden, PD
    Li, S
    INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2001, 38 (15) : 2597 - 2613
  • [45] Dynamic analysis of composite laminates with multiple delamination using improved layerwise theory
    Chattopadhyay, A. (aditi@asu.edu), 1771, American Inst. Aeronautics and Astronautics Inc. (41):
  • [46] Fatigue Delamination Analysis of Composite Laminates with a Central Hole using Interface Elements
    Hosseini-Toudeshky, H.
    Jasemzadeh, A.
    Mohammadi, B.
    COMPOSITE SCIENCE AND TECHNOLOGY, PTS 1 AND 2, 2011, 471-472 : 568 - +
  • [47] Modelling orthotropic viscoelastic behaviour of composite laminates using a coincident element method
    Nallainathan, L
    Mu, XL
    Chiu, WK
    Jones, R
    POLYMERS & POLYMER COMPOSITES, 2003, 11 (08): : 669 - 677
  • [48] Numerical simulation of progressive damage and failure in composite laminates using XFEM/CZM coupled approach
    Higuchi, R.
    Okabe, T.
    Nagashima, T.
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2017, 95 : 197 - 207
  • [49] Modeling of delamination in a stratified composite using a Riemann algorithm
    Aymard, C
    LeRoux, AY
    Priou, P
    JOURNAL DE PHYSIQUE IV, 1997, 7 (C3): : 809 - 814
  • [50] Characterization and modeling of rate effects in the dynamic propagation of mode-II delamination in composite laminates
    Guimard, Jean-Mathieu
    Allix, Olivier
    Pechnik, Nicolas
    Thevenet, Pascal
    INTERNATIONAL JOURNAL OF FRACTURE, 2009, 160 (01) : 55 - 71