Delamination analysis of holed composite laminates using interface elements

被引：4
|
作者：
Hosseini-Toudeshky, H. [1 ]
Jalalvand, M. [1 ]
Mohammadi, B. [1 ]
机构：
[1] Amir Kabir Univ Technol, Dept Aerosp Engn, Tehran, Iran
来源：
MESOMECHANICS 2009 | 2009年 / 1卷 / 01期
关键词：
delamination; interface element; composite; hole; lamianate; STRENGTH;
D O I：
10.1016/j.proeng.2009.06.011
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
In this paper interface element with de-cohesive constitutive law is used to predict the failure load of laminates containing a central hole in which delamination is the dominant failure mode of them. For this purpose, the initiation and propagation of inter-laminar crack are modeled using our in hose FEM code. It is shown that at a certain load step, the interface elements between the two layers of -45 degrees and 0 degrees fail abruptly. It is also shown that the predicted failure stresses of laminates with various thicknesses are in an acceptable agreement with the experimental results. (C) 2009 Elsevier B. V. All rights reserved
引用
收藏
页码：39 / 42
页数：4
相关论文
共 50 条
  • [1] 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 - +
  • [2] Rotational interface formulation for delamination analysis of composite laminates
    Jansson, NE
    Larsson, R
    COMPUTERS & STRUCTURES, 2003, 81 (30-31) : 2705 - 2716
  • [3] Delamination Depth in Composites Laminates With Interface Elements and Ultrasound Analysis
    Amaro, A. M.
    Santos, J. B.
    Cirne, J. S.
    STRAIN, 2011, 47 (02) : 138 - 145
  • [4] Failure probability prediction of delamination under cyclic loading in composite laminates using cohesive interface elements
    Tao, Chongcong
    Zhang, Chao
    Ji, Hongli
    Qiu, Jinhao
    ENGINEERING FRACTURE MECHANICS, 2021, 258
  • [5] Delamination detection in holed CFRP laminates using visualized ultrasound propagation
    Yashiro, Shigeki
    Takatsubo, Junji
    Toyama, Nobuyuki
    Okabe, Tomonaga
    Takeda, Nobuo
    Nihon Kikai Gakkai Ronbunshu, A Hen/Transactions of the Japan Society of Mechanical Engineers, Part A, 2006, 72 (12): : 1882 - 1887
  • [6] Analysis of delamination based interface element with interval method in composite laminates
    Sun, Min
    Qiu, Zhiping
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2010, 27 (02): : 123 - 126
  • [7] Prediction of impact-induced delamination in cross-ply composite laminates using cohesive interface elements
    Aymerich, F.
    Dore, F.
    Priolo, P.
    COMPOSITES SCIENCE AND TECHNOLOGY, 2008, 68 (12) : 2383 - 2390
  • [8] Postbuckling analysis of composite laminates with a delamination
    Kim, Hyo-Jin
    Computers and Structures, 1997, 62 (06): : 975 - 983
  • [9] Postbuckling analysis of composite laminates with a delamination
    Kim, HJ
    COMPUTERS & STRUCTURES, 1997, 62 (06) : 975 - 983
  • [10] Efficient modeling of postbuckling delamination growth in composite laminates using plate elements
    Klug, J
    Wu, XX
    Sun, CT
    AIAA JOURNAL, 1996, 34 (01) : 178 - 184
12345