Numerical Investigation on Dynamic Response of Carbon Fiber Honeycomb Sandwich Panels Subject to Underwater Impact Load

被引:0
|
作者
Zheng, Cheng [1 ]
Wang, Mingfei [1 ,2 ]
Wang, Yiwen [1 ]
Liao, Yawen [1 ,2 ]
Kong, Xiangshao [1 ]
Wu, Weiguo [1 ]
机构
[1] Wuhan Univ Technol, Green & Smart River Sea Going Ship Cruise & Yacht, Wuhan 430063, Peoples R China
[2] Wuhan Univ Technol, Sch Naval Architecture Ocean & Energy Power Engn, Wuhan 430063, Peoples R China
基金
中国国家自然科学基金;
关键词
carbon fiber composites; underwater impact; honeycomb sandwich structures; dynamic response; FAILURE MODES; CORE; OPTIMIZATION; DEFORMATION; PERFORMANCE; DESIGN; DAMAGE; PLATE; BEAMS;
D O I
10.3390/jmse12091513
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
This study investigates the dynamic response and failure mechanisms of carbon fiber honeycomb sandwich structures under underwater impact loads using finite element numerical simulation. The geometric modeling was performed using HyperMesh, and the dynamic response simulations were carried out in ABAQUS, focusing on honeycomb core configurations with varying edge lengths, heights, and gradient forms. The Hashin damage model was employed to describe the damage evolution of the composite materials. The simulation results revealed that the dynamic response was significantly influenced by the initial shock wave pressure and the geometrical parameters of the honeycomb cells. Larger cell-edge lengths and heights generally resulted in improved energy absorption and reduced rear panel displacement. Among the different configurations, interlayer gradient honeycomb structures demonstrated superior impact resistance compared to homogeneous and in-plane gradient structures, particularly under higher initial shock wave pressures. These findings contribute to optimizing the design of carbon fiber honeycomb sandwich structures for enhanced impact resistance in relevant applications.
引用
收藏
页数:24
相关论文
共 50 条
  • [31] Test of composite honeycomb sandwich structure with thin facesheets subject to impact load
    Liu, Longquan, 1600, Beijing University of Aeronautics and Astronautics (BUAA) (31):
  • [32] Experimental and numerical investigation of impact behavior in honeycomb sandwich composites
    Djellab, A.
    Chellil, A.
    Lecheb, S.
    Safi, B.
    Mechakra, H.
    Houari, A.
    Kebir, H.
    Madani, K.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART L-JOURNAL OF MATERIALS-DESIGN AND APPLICATIONS, 2024, 238 (07) : 1342 - 1357
  • [33] Dynamic analysis of aluminium alloy honeycomb core sandwich panels subjected to underwater shock loading
    Ren P.
    Zhang W.
    Liu J.-H.
    Huang W.
    Zhendong yu Chongji/Journal of Vibration and Shock, 2016, 35 (02): : 7 - 11and17
  • [34] The effect of short Kevlar fibers interfacial toughening on impact properties of carbon fiber/aluminum honeycomb sandwich panels
    Wang, Guoxin
    Shi, Shanshan
    Zhao, Zhiting
    Lv, Chaoyu
    Chen, Bingzhi
    Sun, Zhi
    Hu, Xiaozhi
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 155
  • [35] Dynamic response of anisotropic sandwich panels to underwater and in-air explosions
    Librescu, L
    Oh, SY
    Hohe, J
    Sandwich Structures7: Advancing with Sandwich Structures and Materials, 2005, : 97 - 106
  • [36] Numerical Study of Low-Velocity Impact Response of a Fiber Composite Honeycomb Sandwich Structure
    Wen, Zhou
    Li, Ming
    MATERIALS, 2023, 16 (15)
  • [37] Dynamic Response of Bird Strike on Aluminum Honeycomb-Based Sandwich Panels
    Liu, Jun
    Li, Yulong
    Shi, Xiaopeng
    Wang, Wenzhi
    JOURNAL OF AEROSPACE ENGINEERING, 2014, 27 (03) : 520 - 528
  • [38] An experimental investigation of porous volcano rock hypervelocity impact on honeycomb sandwich panels
    Liao G.
    Chen Y.
    Liu X.
    Jia B.
    Zhendong yu Chongji/Journal of Vibration and Shock, 2018, 37 (24): : 1 - 6
  • [39] Dynamic response of bird strike on aluminum honeycomb-based sandwich panels
    Liu, J. (liujun_top@126.com), 1600, American Society of Civil Engineers (ASCE), United States (27):
  • [40] Research on Thermal Load Response Spectrum of FBG Sensors Implanted in Carbon Fiber Honeycomb Sandwich Structure
    Ma Chi
    Zeng Jie
    Zhang Jing-chuan
    Gong Xiao-jing
    Zhang Yi-xin
    Feng Xiang-yu
    Zhou Lin
    SPECTROSCOPY AND SPECTRAL ANALYSIS, 2017, 37 (09) : 2927 - 2932