Tensile characterization of composite honeycomb core sandwich panels after low velocity impact

被引：0
|
作者：
Kou, Changhe
Cheng, Xiaoquan
Li, Zhengneng
机构：
来源：
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | / 15卷 / 04期
关键词：
Laminated composites - Honeycomb structures - Impact testing - Tensile strength - Failure (mechanical);
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Tensile tests after velocity impact were carried out on honeycomb core sandwich specimens. Some methods were used to study the cause of tensile failure: X ray, deeply and visual inspection. The relationship between residual tensile strength and impact energy was analyzed. The results show that in the course of tension, four failure modes existed meanwhile and interacted each other. Impact damage affected the tensile ability of honeycomb core sandwich panel.
引用
收藏
页码：69 / 73
相关论文
共 50 条
  • [1] Tensile characterization of composite honeycomb core sandwich panels after low velocity impact
    Kou, Changhe
    Cheng, Xiaoquan
    Li, Zhengneng
    Kang T'ieh/Iron and Steel (Peking), 1998, 33 (10): : 69 - 73
  • [2] Study on damage of composite honeycomb core sandwich panels under low velocity impact
    Beijing Univ of Aeronautics &, Astronautics, Beijing, China
    Fuhe Cailiao Xuebao, 3 (124-128):
  • [3] Prediction of the compressive strength for composite honeycomb core sandwich panels after low speed impact
    Kou, Changhe
    Cheng, Xiaoquan
    Li, Zhengneng
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 1998, 24 (05): : 555 - 558
  • [4] Simulation of Low Velocity Impact of Honeycomb Sandwich Composite Panels for the BIMODAL Tram Application
    Lee, Jae Youl
    Shin, Kwang Bok
    Jeong, Jong Cheol
    COMPOSITES RESEARCH, 2007, 20 (04): : 42 - 50
  • [5] An analytical model for composite sandwich panels with honeycomb core subjected to high-velocity impact
    Feli, S.
    Pour, M. H. Namdari
    COMPOSITES PART B-ENGINEERING, 2012, 43 (05) : 2439 - 2447
  • [6] Damage Characterization of Polypropylene Honeycomb Sandwich Panels Subjected to Low-Velocity Impact
    Amir, Freeda A.
    Othman, A. R.
    Akil, H. Md.
    ADVANCES IN MATERIALS SCIENCE AND ENGINEERING, 2013, 2013
  • [7] A Study on Low-Velocity Impact Characterization of Honeycomb Sandwich Panels According to the Changes of Impact Location and Core Fabrication Angles
    Jeon, Kwang-Woo
    Shin, Kwang-Bok
    Ko, Hee-Young
    Kim, Dae-Hwan
    TRANSACTIONS OF THE KOREAN SOCIETY OF MECHANICAL ENGINEERS A, 2009, 33 (01) : 64 - 71
  • [8] On the structural parameters of honeycomb-core sandwich panels against low-velocity impact
    Sun, Guangyong
    Huo, Xintao
    Wang, Hongxu
    Hazell, Paul J.
    Li, Qing
    COMPOSITES PART B-ENGINEERING, 2021, 216
  • [9] Damage propagation behavior of composite honeycomb sandwich panels under low-velocity impact
    Xie, Zonghong
    Su, Ni
    Zhang, Lei
    Zhao, Jian
    Li, Lei
    Wei, Hongyan
    Wang, Jian
    Yang, Shengchun
    Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics, 2009, 41 (01): : 30 - 35
  • [10] Damage analysis of honeycomb core composite sandwich rate subjected low velocity impact
    Zheng, QX
    Li, ZN
    Wu, D
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2000, 19 (01) : 58 - 68
12345