剪切载荷作用下含损伤胶接材料界面动应力强度因子的研究

蔡艳红; 陈浩然; 唐立强; 闫澄; 江莞

剪切载荷作用下含损伤胶接材料界面动应力强度因子的研究

1.
大连理工大学工业装备结构分析国家重点实验室,辽宁大连 116024;2.哈尔滨工程大学建筑工程学院,哈尔滨 150001;3.昆士兰理工大学环境与工程学部,布里斯班,QLD 4001 澳大利亚;4.中国科学院上海硅酸盐研究所高性能陶瓷和超微结构国家重点实验室,上海 200050

基金项目: 国家自然科学基金资助项目(10672027);国家重大基础研究计划(973)资助项目(2006CB601205);国家杰出青年基金资助项目(50625414)

详细信息

作者简介:
蔡艳红(1969- ),女,黑龙江人,讲师,博士;陈浩然(1940- ),男,教授,博士生导师(联系人.Tel:+86-411-84706348;E-mail:chenhr@dlut.edu.cn).

中图分类号: O346.1
计量
- 文章访问数: 3301
- HTML全文浏览量: 160
- PDF下载量: 802
- 被引次数: 0
出版历程
- 收稿日期: 2007-08-17
- 修回日期: 2008-09-26
- 刊出日期: 2008-11-15

Dynamic Stress Intensity Factor Analysis of Adhesively Bonded Material Interface With Damage Under Shear Loading

1.
State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian, Liaoning 116024, P. R. China;

摘要

摘要: 主要针对剪切载荷作用下，胶接材料接合区域界面裂纹尖端动态应力强度因子进行了分析，其中考虑了裂尖区域的损伤．通过积分变换，引入位错密度函数，奇异积分方程被简化为代数方程，并采用配点法求解；最后经过Laplace逆变换，得到动态应力强度因子的时间响应．Ⅱ型动应力强度因子随着黏弹性胶层的剪切松弛参量、弹性基底的剪切模量和Poisson比的增加而增大；随膨胀松弛参量的增加而减小．损伤屏蔽发生在裂纹扩展的起始阶段．裂纹尖端的奇异性指数(-0.5)是与材料参数、损伤程度和时间无关的，而振荡指数由黏弹性材料参数控制．
- 动态应力强度因子 /
- 界面裂纹 /
- 胶接材料 /
- 损伤 /
- 奇异积分方程
Abstract: The dynamic stress intensity factor (DSIF) at the interface in an adhesive joint under shear loading is investigated. The material damage was considered. By introducing dislocation density function and using integral transform, the problem was reduced to algebraic equations and could be solved with collocation dots method in the Laplace domain. Finally, the time response of DSIF was calculated with the inverse Laplace integral transform. The conclusions show that the mode Ⅱ DSIF increases with the shear relaxation parameter, shear module and Poisson ratio, but decreases with swell relaxation parameter. Damage shielding only occurs at the initial stage of crack propagation. The singular index of crack tip is 0.5 and independent of the material parameters and damage conditions of materials and time. The oscillatory index is controlled by viscoelastic material parameters.
- dynamic stress intensity factor /
- interface crack /
- adhesively bonded material /
- damage /
- singular integral equation

HTML全文

参考文献(20)

[1]	张丽新,杨士勤,何世禹，等. 在空间环境因素作用下胶接材料的损伤行为[J]. 中国胶粘剂,2001,10(4):42-48.
[2]	Choupani Naghdali. Interfacial mixed-mode fracture characterization of adhesively bonded joints[J].International Journal of Adhesion & Adhesives，2008,28(6):267-282.
[3]	Goyal Vinay K, Johnson Eric R,Goyal Vijay K. Predictive strength-fracture model for composite bonded joints[J].Composite Structures,2008,82(3): 434-446. doi: 10.1016/j.compstruct.2007.01.029
[4]	Liljedahl C D M, Crocombe A D, Wahab M A,et al.Modelling the environmental degradation of adhesively bonded aluminium and composite joints using a CZM approach[J].International Journal of Adhesion & Adhesives,2007,27(6):505-518.
[5]	Casas-Rodriguez J P, Ashcroft I A,Silberschmidt V V. Damage in adhesively bonded CFRP joints: Sinusoidal and impact-fatigue[J].Composites Science and Technology,2008, DOI: 10.1016/j.compscitech.2008.04.030.
[6]	Roberta Rizza, Kevinb Meade. No-slip crack model for damaged bone/cement interface[J].Engineering Fracture Mechanics,2003,70(6):757-773. doi: 10.1016/S0013-7944(02)00085-1
[7]	Papanikos P, Tserpes K I, Labeas G,et al.Progressive damage modelling of bonded composite repairs[J].Theoretical and Applied Fracture Mechanics,2005,43(2):189-198. doi: 10.1016/j.tafmec.2005.01.004
[8]	Nayeb-Hashemi H, Swet D,Vaziri A.New electrical potential method for measuring crack growth in nonconductive materials[J].Measurement,2004,36(2):121-129. doi: 10.1016/j.measurement.2004.05.002
[9]	Guo T F, Cheng L. Vapor pressure and void size effects on failure of a constrained ductile film [J].Journal of the Mechanics and Physics of Solids,2003,51(6):993-1014. doi: 10.1016/S0022-5096(03)00007-3
[10]	Xu L Roy, Rosakis Ares J.An experimental study of impact-induced failure events in homogeneous layered materials using dynamic photoelasticity and high-speed photography[J].Optics and Lasers in Engineering,2003,40(4):263-288. doi: 10.1016/S0143-8166(02)00093-3
[11]	张凤鹏，黄宝宗.复合材料层板分层尖端微裂纹损伤演变分析[J].高压物理学报. 1999，13(增刊):349-352.
[12]	刘忠. 考虑裂尖损伤的黏弹性裂纹扩展规律[J]. 湘潭大学自然科学学报,1997, 19(2):38-42.
[13]	黄西成. 聚合物材料损伤理论[J].应用数学和力学,1999,19(3):325-329.
[14]	樊建平，沈为，彭立华. 树脂基复合材料蠕变损伤本构方程[J]. 华中理工大学学报,1996,24(增刊(Ⅱ)):100-102.
[15]	蔡艳红，陈浩然，王灿. 无限长条板中弹性与黏弹性界面裂纹尖端场[J]. 复合材料学报,2005,22(6): 156-164.
[16]	Erdogan F. Mixed boundary value problems[J].Mechanics Today,1978,6(4):1-86.
[17]	Wwi P J,Zhang S Y. Singularity of dynamic stress fields around an interface crack between viscoelastic bodies [J].International Journal of Fracture,2004,126(2):165-177. doi: 10.1023/B:FRAC.0000026361.01552.80
[18]	Erdogan F, Gupta G D, Cook T S.Numerical solution of singular integral equation[A].In: G C Sih,Ed.Mechanics of Fracture 1, Methods of Analysis and Solutions of Crack Problems[C].Noordhoff, Leyden: International Publishing, 1973, 368-425.
[19]	Erdogan F, Wu B H. Crack problem in FGM layers under thermal stresses[J].J Thermal Stresses,1996,19(3):237-265. doi: 10.1080/01495739608946172
[20]	Rice J. Elastic fracture mechanics concepts for interfacial cracks[J].J Appl Mech,1988,55(1):98-103. doi: 10.1115/1.3173668

施引文献

资源附件(0)

访问统计

计量

文章访问数: 3301
HTML全文浏览量: 160
PDF下载量: 802
被引次数: 0

姓名
邮箱
手机号码
标题
留言内容
验证码

留言板

剪切载荷作用下含损伤胶接材料界面动应力强度因子的研究

作者简介:
蔡艳红(1969- ),女,黑龙江人,讲师,博士;陈浩然(1940- ),男,教授,博士生导师(联系人.Tel:+86-411-84706348;E-mail:chenhr@dlut.edu.cn).

计量

Dynamic Stress Intensity Factor Analysis of Adhesively Bonded Material Interface With Damage Under Shear Loading

计量

目录

留言板

剪切载荷作用下含损伤胶接材料界面动应力强度因子的研究

作者简介: 蔡艳红(1969- ),女,黑龙江人,讲师,博士;陈浩然(1940- ),男,教授,博士生导师(联系人.Tel:+86-411-84706348;E-mail:chenhr@dlut.edu.cn).

计量

出版历程

Dynamic Stress Intensity Factor Analysis of Adhesively Bonded Material Interface With Damage Under Shear Loading

计量

出版历程

目录

作者简介:
蔡艳红(1969- ),女,黑龙江人,讲师,博士;陈浩然(1940- ),男,教授,博士生导师(联系人.Tel:+86-411-84706348;E-mail:chenhr@dlut.edu.cn).