Experimental and FEM studies on mechanical properties of single-lap adhesive joint with dissimilar adherends subjected to impact tensile loadings

被引:37
|
作者
Liao, Lijuan [1 ]
Sawa, Toshiyuki [2 ]
Huang, Chenguang [1 ]
机构
[1] Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China
[2] Hiroshima Univ, Grad Sch Engn, Higashihiroshima, Hiroshima 7398527, Japan
基金
中国国家自然科学基金;
关键词
Single-lap adhesive joints; Dissimilar adherends; Impact tensile loadings; Interface stress distributions; Stress wave propagations; ELEMENT STRESS-ANALYSIS; BUTT JOINTS; STRENGTH EVALUATION; HOLLOW CYLINDERS; BONDED JOINTS; DEFORMATION;
D O I
10.1016/j.ijadhadh.2013.02.007
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
The rupture initiation position, the stress wave propagations and interface stress distributions of the single-lap adhesive joint with dissimilar adherends under impact tensile loadings are analyzed via experiments combined with FEM calculations taking account of the strain rate dependency property of the adhesive. It is obtained that rupture initiates at the interface of the adherend with higher Young's modulus (steel side in this study) in the joint under impact tensile loadings, which shows the opposite characteristic in the same type of joint under static loadings. A fairly good agreement is observed between the experimental measured and FEM calculated results. In addition, it is also found that the strength of the joint with dissimilar adherends is smaller than that of the joint with similar adherends when the joint is subjected to the impact tensile loadings owing to the different extent of the wave impedance mismatch which depends on the material properties. Finally, the design guideline for the single-lap adhesive joint is summarized and provided. (c) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:91 / 98
页数:8
相关论文
共 50 条
  • [21] Numerical and Experimental Analysis of Balanced and Unbalanced Adhesive Single-Lap Joints between Aluminium Adherends
    Pinto, A. M. G.
    Campilho, R. D. S. G.
    Mendes, I. R.
    Baptista, A. P. M.
    JOURNAL OF ADHESION, 2014, 90 (01): : 89 - 103
  • [22] Numerical Study of Adhesive Single-Lap Joints with Composite Adherends Subjected to Combined Tension-Torsion Loads
    Khalili, S. M. R.
    Mokhtari, M.
    JOURNAL OF ADHESION, 2015, 91 (03): : 214 - 234
  • [24] A two-dimensional stress analysis of single-lap adhesive joints subjected to tensile loads
    Department of Mechanical Engineering, Yamanashi University, 4-3-11, Takeda, Kofu, Yamanashi 400, Japan
    不详
    不详
    J Adhes Sci Technol, 8 (1039-1062):
  • [25] A two-dimensional stress analysis of single-lap adhesive joints subjected to tensile loads
    Sawa, T
    Nakano, K
    Toratani, H
    JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 1997, 11 (08) : 1039 - 1062
  • [26] Effect of fiber layup methods on tensile properties of CFRP-aluminum alloy single-lap adhesive joint
    Zou T.
    Li L.
    Fu J.
    Li Y.
    Ju Y.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2022, 37 (09): : 1905 - 1914
  • [27] Tensile properties of a composite–metal single-lap hybrid bonded/bolted joint
    Xiaoqi LI
    Xiaoquan CHENG
    Yujia CHENG
    Zhiyong WANG
    Wenjun HUANG
    Chinese Journal of Aeronautics, 2021, 34 (02) : 629 - 640
  • [28] Two-dimensional stress analysis of single-lap adhesive joints subjected to tensile shear loads
    Nippon Kikai Gakkai Ronbunshu, A Hen/Transactions of the Japan Society of Mechanical Engineers, Part A, 1995, 61 (589): : 1994 - 2002
  • [29] Tensile properties of a composite?metal single-lap hybrid bonded/bolted joint
    LI, Xiaoqi
    CHENG, Xiaoquan
    CHENG, Yujia
    WANG, Zhiyong
    HUANG, Wenjun
    CHINESE JOURNAL OF AERONAUTICS, 2021, 34 (02) : 629 - 640
  • [30] Three-dimensional FEM stress analysis and strength prediction of scarf adhesive joints with similar adherends subjected to static tensile loadings
    Nakano, Hiroko
    Omiya, Yuya
    Sekiguchi, Yasuhisa
    Sawa, Toshiyuki
    INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2014, 54 : 40 - 50