Modeling on mechanical behavior and damage evolution of single-lap bolted composite interference-fit joints under thermal effects

被引:0
|
作者
Junshan HU [1 ]
Kaifu ZHANG [2 ]
Hui CHENG [2 ]
Peng ZOU [3 ]
机构
[1] 不详
[2] College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics and Astronautics
[3] 不详
[4] School of Mechanical Engineering, Northwestern Polytechnical University
[5] Aircraft Strength Research Institute of China
[6] 不详
关键词
D O I
暂无
中图分类号
V26 [航空制造工艺];
学科分类号
082503 ;
摘要
This paper reports the modeling method and outcomes of mechanical performance and damage evolution of single-lap bolted composite interference-fit joints under extreme temperatures.The anisotropic continuum damage model involving thermal effects is established on continuum damage mechanics which integrates the shear nonlinearity constitutive relations characterized by Romberg-Osgood equation. The temperature-induced modification of thermal strains and material properties is incorporated in stress-strain analysis, extended 3 D failure criteria and exponential damage evolution rules. The proposed model is calibrated and employed to simulate behavior of composite joints in interference fitting, bolt preloading, thermal and bearing loading processes, during which the influence of interference-fit sizes, preload levels, laminate layups and service temperatures is thoroughly investigated. The predicated interfacial behavior, bearing response and failure modes are in good agreement with experimental tests. The numerical model is even capable of reflecting some non-intuitive experimental findings such as residual stress relaxation and matrix softening at elevated temperatures.
引用
收藏
页码:230 / 244
页数:15
相关论文
共 50 条
  • [41] Improving load sharing in hybrid bonded/bolted composite joints using an interference-fit bolt
    Raju, Karthik Prasanna
    Bodjona, Kobye
    Lim, Gyu-Hyeong
    Lessard, Larry
    COMPOSITE STRUCTURES, 2016, 149 : 329 - 338
  • [42] Experimental investigations of bolted, adhesively bonded and hybrid bolted/bonded single-lap joints in composite laminates
    Li, Xin
    Tan, Zhiyong
    Wang, Lechen
    Zhang, Jian
    Xiao, Zhen
    Luo, Haibo
    MATERIALS TODAY COMMUNICATIONS, 2020, 24
  • [43] Damage progression and failure of single-lap thin-ply laminated composite bolted joints under quasi-static loading
    Cao, Yuejie
    Cao, Zengqiang
    Zhao, Y.
    Zuo, Duquan
    Tay, T. E.
    INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2020, 170
  • [44] An analytical model for the secondary bending prediction in single-lap composite bolted-joints
    Olmedo, A.
    Santiuste, C.
    Barbero, E.
    COMPOSITE STRUCTURES, 2014, 111 : 354 - 361
  • [45] Effect of bolt preload on bearing response of single-lap, countersunk composite bolted joints
    Li, Rupeng
    Xiao, Ruiheng
    Ge, Ende
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2024, 41 (07): : 3765 - 3776
  • [46] Mesoscale modelling of progressive damage and failure in single-lap and double-lap thin-ply laminated composite bolted joints
    Cao, Yuejie
    Zhi, Jie
    Zuo, Duquan
    Li, Xiang
    Cao, Zengqiang
    Wang, Yonghu
    Tay, T. E.
    COMPOSITE STRUCTURES, 2023, 316
  • [47] A Damage Model for Adhesively Bonded Single-Lap Thick Composite Joints
    Nassar, Sayed A.
    Mao, Jianghui
    Yang, Xianjie
    Templeton, Douglas
    JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 2012, 134 (04):
  • [48] Fatigue strength assessment of an interference fit of single-bolt, double shear lap composite bolted joints
    Wang, F.-L. (wangfl@vip.sina.com), 2012, Tsinghua University (29):
  • [49] Analysis of bolted-bonded composite single-lap joints under combined in-plane and transverse loading
    Barut, A.
    Madenci, E.
    COMPOSITE STRUCTURES, 2009, 88 (04) : 579 - 594
  • [50] Evaluation of typical hole-making strategies on mechanical behavior of CFRP/Ti single-lap bolted joints
    Zou, Fan
    Dang, Jiaqiang
    Chen, Tao
    An, Qinglong
    Chen, Ming
    COMPOSITE STRUCTURES, 2023, 305