Modelling impact damage in marine composite panels

被引:56
|
作者
Johnson, H. E. [1 ]
Louca, L. A. [1 ]
Mouring, S. [2 ]
Fallah, A. S. [1 ]
机构
[1] Univ London Imperial Coll Sci Technol & Med, Dept Civil & Environm Engn, London SW7 2AZ, England
[2] USN Acad, Dept Naval Architecture & Ocean Engn, Annapolis, MD 21402 USA
基金
英国工程与自然科学研究理事会;
关键词
Woven composites; Impact; Finite element; Damage mechanics; Delamination; FIBER-REINFORCED COMPOSITES; LAMINATED COMPOSITES; POLYMER COMPOSITES; CONSTITUTIVE MODEL; STRAIN RATES; WOVEN GLASS; PART I; FAILURE; DELAMINATION; MECHANICS;
D O I
10.1016/j.ijimpeng.2008.01.013
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In order to establish the survivability of a composite structure under a dynamic load, it is important to be able to predict the damage incurred and the effect of the contact force. The damage caused by low velocity impact is often hidden and for thicker plates the transverse stresses are significant in promoting delamination. In this study, woven vinyl-ester composite plates up to 1.37 m long are numerically modelled with a simple, gradually damaging three-dimensional material model and the results are compared with full-scale tests. The model is based on damage mechanics principles using cyclic test data to obtain modulus reduction with damage. Delamination is modelled with a mixed-mode traction-separation law using cohesive elements. The nonlinear elastic orthotropic material model for the woven plies is written in a VUMAT in Abaqus/Explicit and the effects of varying some of the modelling parameters are briefly discussed through the examination of the contact force. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:25 / 39
页数:15
相关论文
共 50 条
  • [31] Influence of loading conditions on the impact damage resistance of composite panels
    Riccio, A
    Tessitore, N
    COMPUTERS & STRUCTURES, 2005, 83 (28-30) : 2306 - 2317
  • [32] Modelling damage evolution in composite laminates subjected to low velocity impact
    Shi, Y.
    Swait, T.
    Soutis, C.
    COMPOSITE STRUCTURES, 2012, 94 (09) : 2902 - 2913
  • [33] Modelling impact damage in composite laminates: A simulation of intra- and inter-laminar cracking
    Shi, Y.
    Pinna, C.
    Soutis, C.
    COMPOSITE STRUCTURES, 2014, 114 : 10 - 19
  • [34] Weight optimisation of damage resistant composite panels with a posteriori cost evaluation
    Gigliotti, Marco
    Riccio, Aniello
    Luspa, Luigi
    Scaramuzzino, Francesco
    Mormile, Luigi
    COMPOSITE STRUCTURES, 2009, 88 (02) : 312 - 322
  • [35] Engineering method for prediction of impact response and damage in sandwich panels
    Olsson, R
    JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2002, 4 (01) : 3 - 29
  • [36] Prediction of fatigue damage for composite laminate using impact response
    Kim, Sung Joon
    Hwang, In Hee
    INTERNATIONAL JOURNAL OF FATIGUE, 2006, 28 (10) : 1334 - 1339
  • [37] Impact damage of composite laminates with high-speed waterjet
    Hou, Naidan
    Zhao, Renxi
    Li, Jian
    Wang, Xuan
    Li, Xi
    Cui, Hao
    Li, Yulong
    INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2022, 167
  • [38] On stability and damage behavior of asymmetric sandwich panels under uniaxial compression
    Deng, Jian
    Peng, Ang
    Chen, Wei
    Zhou, Guangming
    Wang, Xinwei
    JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2021, 23 (06) : 1870 - 1901
  • [39] Strain-rate-dependent progressive damage modelling of UHMWPE composite laminate subjected to impact loading
    Mansoori, Hassan
    Zakeri, Mahnaz
    INTERNATIONAL JOURNAL OF DAMAGE MECHANICS, 2022, 31 (02) : 215 - 245
  • [40] Effects of impact energy, velocity, and impactor mass on the damage induced in composite laminates and sandwich panels
    Aryal, B.
    Morozov, E., V
    Wang, H.
    Shankar, K.
    Hazell, P. J.
    Escobedo-Diaz, J. P.
    COMPOSITE STRUCTURES, 2019, 226