Plasticity induced crack closure in adhesively bonded joints under fatigue loading

被引:16
作者
Donough, M. J. [1 ,2 ]
Gunnion, A. J. [2 ,3 ]
Orifici, A. C. [1 ]
Wang, C. H. [1 ]
机构
[1] RMIT Univ, Sir Lawrence Wackett Aerosp Res Ctr, Sch Aerosp Mech & Mfg Engn, Melbourne, Vic 3001, Australia
[2] Cooperat Res Ctr Adv Composite Struct, Port Melbourne, Vic 3207, Australia
[3] Adv Composite Struct Australia, Port Melbourne, Vic 3207, Australia
关键词
Fatigue debonding; Crack closure; Bonded joints; FINITE-ELEMENT-ANALYSIS; VARIABLE AMPLITUDE FATIGUE; COMPOSITE JOINTS; MODE-I; DELAMINATION GROWTH; FRACTURE-TOUGHNESS; CONSTRAINED LAYERS; STRESS; THICKNESS; CONSTANT;
D O I
10.1016/j.ijfatigue.2014.07.003
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The mean load of a cyclic loading has a large effect on fatigue crack growth rates in metallic materials and bonded joints. In metallic structures, this effect has been attributed to plasticity-induced crack closure, but little is known about the mechanism responsible for this mean load effect on fatigue crack growth in adhesively bonded joints. This paper presents a computational investigation of the plasticity-induced crack closure mechanism affecting disband growth in adhesively bonded joints under fatigue loading. The results show that the ratios of crack-opening and crack-closure are approximately independent of the level of plastic constraint, indicated by the ratio between the plastic zone size and the adhesive thickness. An effective strain-energy release rate parameter, which accounts for the crack closure behaviour, has been developed as a new correlating parameter for disbond growth. Comparisons with the experimental results pertinent to four different adhesive bonded joints reveal that this new correlating parameter is capable of unifying the fatigue growth rates by eliminating the effect of mean loads. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:440 / 450
页数:11
相关论文
共 42 条
  • [1] Anderson T.L., 2005, Fracture Mechanics: Fundamentals and Applications, V3rd, P640
  • [2] Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates
    Andersons, J
    Hojo, M
    Ochiai, S
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2004, 26 (06) : 597 - 604
  • [3] Mode I fracture of epoxy bonded composite joints - 2. Fatigue loading
    Ashcroft, IA
    Shaw, SJ
    [J]. INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2002, 22 (02) : 151 - 167
  • [4] Effect of adhesive thickness on fatigue and fracture of toughened epoxy joints - Part I: Experiments
    Azari, S.
    Papini, M.
    Spelt, J. K.
    [J]. ENGINEERING FRACTURE MECHANICS, 2011, 78 (01) : 153 - 162
  • [5] Fatigue threshold behavior of adhesive joints
    Azari, S.
    Papini, M.
    Schroeder, J. A.
    Spelt, K.
    [J]. INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2010, 30 (03) : 145 - 159
  • [6] Crocombe AD, 1999, INT J ADHES ADHES, V19, P19
  • [7] Elber W., 1970, Engineering Fracture Mechanics, V2, P37, DOI 10.1016/0013-7944(70)90028-7
  • [8] A study of adhesively bonded joints subjected to constant and variable amplitude fatigue
    Erpolat, S
    Ashcroft, IA
    Crocombe, AD
    Abdel-Wahab, MM
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2004, 26 (11) : 1189 - 1196
  • [9] Fatigue crack growth acceleration due to intermittent overstressing in adhesively bonded CFRP joints
    Erpolat, S
    Ashcroft, IA
    Crocombe, AD
    Abdel-Wahab, MM
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2004, 35 (10) : 1175 - 1183
  • [10] FAA: Federal Aviation Administration, 2010, AC20107B FAA