Simulation of impact force and energy response of composite laminate subjected to low velocity impact

被引:0
|
作者
School of Aeronautics and Astronautics, Shanghai Jiaotong University, Shanghai [1 ]
200240, China
机构
[1] Tan, Jianshe
[2] Zhang, Xiaojing
[3] Zhang, Junqi
[4] Wang, Hai
来源
Zhang, Xiaojing | 1600年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 31期
关键词
Velocity - Laminated composites - Carbon fiber reinforced plastics - Energy dissipation;
D O I
暂无
中图分类号
学科分类号
摘要
Based on continuum damage mechanics (CDM) approach, a progressive damage model is proposed to predict the impact force and energy response of the carbon fiber-reinforced polymer (CFRP) laminates subjected to low velocity impact. The typical failure modes were simulated by employing damage mode-based failure criteria, irreversible damage variables and computing method of internal energy were defined in order to quantify damage associated with the gradual stiffness reduction and energy dissipation. A good agreement was found between the numerical simulation and experimental results. In addition, the difference between the Hashin criterion and LaRC04 criterion were analyzed, and a combined criterion composed of Hashin and LaRC04 criterion was advised for composite laminates subjected to low velocity impact. Comparison between the Hashin criterion and combined criterion indicates that when there is a lot of compressive failure damage in CFRP composite laminates, combined criterion is more suitable for the case in this paper, and a conservative result would be obtained if Hashin criterion is adopted.
引用
收藏
相关论文
共 50 条
  • [41] Modelling damage evolution in composite laminates subjected to low velocity impact
    Shi, Y.
    Swait, T.
    Soutis, C.
    COMPOSITE STRUCTURES, 2012, 94 (09) : 2902 - 2913
  • [42] PREDICTION OF DELAMINATION IN COMPOSITE LAMINATES SUBJECTED TO LOW-VELOCITY IMPACT
    JIH, CJ
    SUN, CT
    JOURNAL OF COMPOSITE MATERIALS, 1993, 27 (07) : 684 - 701
  • [43] Delamination growth analysis in composite laminates subjected to low velocity impact
    Kharazan, Masoud
    Sadr, M. H.
    Kiani, Morteza
    STEEL AND COMPOSITE STRUCTURES, 2014, 17 (04): : 387 - 403
  • [44] Theoretical and numerical analyses of composite cylinders subjected to the low velocity impact
    Rafiee, Roham
    Ghorbanhosseini, Amin
    Rezaee, Shiva
    COMPOSITE STRUCTURES, 2019, 226
  • [45] Peridynamic modeling of composite laminate under low-velocity impact using energy-based criteria
    Jiang X.
    Wang H.
    Zhu J.
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2024, 41 (04): : 2126 - 2136
  • [46] Influence of laminate thickness and impactor shape on low velocity impact response of jute -epoxy composite: FE study
    Mahesh, Vishwas
    Joladarashi, Sharnappa
    Kulkarni, Satyabodh M.
    MATERIALS TODAY-PROCEEDINGS, 2020, 28 : 545 - 550
  • [47] Quasi-static simulation of composite-laminated shells subjected to low-velocity impact
    Huang, CH
    Lee, YJ
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2005, 24 (07) : 763 - 774
  • [48] Polymer-matrix composites subjected to low-velocity impact: effect of laminate configuration
    Naik, NK
    Meduri, S
    COMPOSITES SCIENCE AND TECHNOLOGY, 2001, 61 (10) : 1429 - 1436
  • [49] Contact-impact analysis of laminated composite structures subjected to low-velocity impact
    Li, Wei
    Ye, TianqI
    Zhang, Yinig
    Yang, Xu
    Jixie Kexue Yu Jishu/Mechanical Science and Technology, 1996, 15 (01):
  • [50] Failure mechanisms of composite laminate subjected to edge-on impact
    Zhong X.
    Li Z.
    Li N.
    Ye Q.
    Ju C.
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2023, 40 (10): : 5932 - 5946