Finite Element Analysis of Crack Propagation in Adhesive Joints with Notched Adherends

被引:3
|
作者
Qureshi, Ayman [1 ]
Guan, Tianyue [1 ]
Alfano, Marco [1 ]
机构
[1] Univ Waterloo, Dept Mech & Mechatron Engn, 200 Univ Ave West, Waterloo, ON N2L 3G1, Canada
基金
加拿大自然科学与工程研究理事会;
关键词
adhesive joints; DCB; cohesive zone model; crack growth; toughening; snap-through; SINGLE LAP JOINTS; COHESIVE ZONE; LASER-ABLATION; FRACTURE;
D O I
10.3390/ma16010391
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
The adherends notching technique has been the subject of a few recent studies and consists of tailoring the geometry of the adjoined layers to mitigate the bondline peak stresses and enhance the joint strength. In the present study, we explored the effect of the adherends notching technique on crack propagation using finite element (FE) simulations based on the cohesive zone model (CZM) of fracture. Double cantilever beam (DCB) adhesive joints subjected to quasistatic loading were considered as a model material system. An array of equally spaced notches was placed on the faying sides of the adherends, oriented perpendicularly to the direction of crack growth. A parametric investigation was carried out to ascertain the role of the notches and the input cohesive properties on various performance metrics, e.g., load-displacement response and dissipated energy. The proposed notching strategy promotes an unstable crack pinning/depinning process, which effectively delays crack growth and increases the effective work of fracture. Additionally, we found that the overall behaviour is tunable by changing geometric (i.e., notch spacing and depth) and bondline material properties.
引用
收藏
页数:16
相关论文
共 50 条
  • [1] Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends II. Finite element analysis
    Guild, F.J.
    Potter, K.D.
    Heinrich, J.
    Adams, R.D.
    Winsom, M.R.
    1600, Elsevier Ltd (21):
  • [2] Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends II. Finite element analysis
    Guild, FJ
    Potter, KD
    Heinrich, J
    Adams, RD
    Wisnom, MR
    INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2001, 21 (06) : 445 - 453
  • [3] Global-Local Finite Element Analysis of Adhesive Joints and Crack Propagation
    Islam, Mohammad M.
    Kapania, Rakesh K.
    JOURNAL OF AIRCRAFT, 2014, 51 (01): : 310 - 319
  • [4] Finite Element Analysis of Single-lap Adhesive Joints with Tapered Adherends
    Marchione, F.
    INTERNATIONAL JOURNAL OF ENGINEERING, 2021, 34 (10): : 2213 - 2218
  • [5] A finite element analysis of crack initiation and propagation in a notched disk submitted to rolling contact fatigue
    Bordi, V
    Dorier, C
    Villechaise, B
    JOURNAL OF TRIBOLOGY-TRANSACTIONS OF THE ASME, 1998, 120 (03): : 436 - 441
  • [6] Finite-element stress response analysis of adhesive scarf joints of dissimilar adherends subjected to impact tensile loads
    Shimura, Jyo
    Hirashima, Ken-Ichi
    Yosetsu Gakkai Ronbunshu/Quarterly Journal of the Japan Welding Society, 2002, 20 (01): : 128 - 135
  • [8] Finite element analysis of fretting crack propagation
    Proudhon, H.
    Basseville, S.
    ENGINEERING FRACTURE MECHANICS, 2011, 78 (04) : 685 - 694
  • [9] Nonlinear viscoelastic finite element analysis of adhesive joints
    Roy, S.
    Reddy, J.N.
    Tire Science and Technology, 1988, 16 (03) : 146 - 170
  • [10] ANALYSIS OF ADHESIVE-BONDED JOINTS WITH NONIDENTICAL ADHERENDS
    CHENG, S
    CHEN, D
    SHI, YP
    JOURNAL OF ENGINEERING MECHANICS, 1991, 117 (03) : 605 - 623