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] Detection of Impact Damage in Composite Panels using Guided Ultrasonic Waves
    Murat, Bibi Intan Suraya
    Fromme, Paul
    HEALTH MONITORING OF STRUCTURAL AND BIOLOGICAL SYSTEMS 2013, 2013, 8695
  • [32] Modelling of impact damage zones in composite laminates for strength after impact
    Olsson, R.
    AERONAUTICAL JOURNAL, 2012, 116 (1186): : 1349 - 1365
  • [33] Low velocity impact modelling in laminate composite panels with discrete interface elements
    Bouvet, Christophe
    Castanie, Bruno
    Bizeul, Matthieu
    Barrau, Jean-Jacques
    INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2009, 46 (14-15) : 2809 - 2821
  • [34] DAMAGE TOLERANCE OF COMPOSITE SHEAR PANELS
    LLORENTE, S
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1989, 34 (02) : 43 - 51
  • [35] Progressive damage of unidirectional composite panels
    Las, Vladislav
    Zemcik, Robert
    JOURNAL OF COMPOSITE MATERIALS, 2008, 42 (01) : 25 - 44
  • [36] IMPACT DAMAGE RESPONSE OF CARBON FIBRE-REINFORCED AEROSPACE COMPOSITE PANELS
    Nezhad, Hamed Yazdani
    Auffray, Anthony
    McCarthy, Conor T.
    O'Higgins, Ronan
    20TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS, 2015,
  • [37] Damage prediction in composite sandwich panels subjected to low-velocity impact
    Feng, D.
    Aymerich, F.
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2013, 52 : 12 - 22
  • [38] Detection and Characterization of Impact Damage in Composite Panels using Multiple Ultrasonic Methods
    Williams, Westin B.
    Michaels, Thomas E.
    Michaels, Jennifer E.
    41ST ANNUAL REVIEW OF PROGRESS IN QUANTITATIVE NONDESTRUCTIVE EVALUATION, VOL 34, 2015, 1650 : 1239 - 1246
  • [39] Behavior of compression-loaded composite panels with stringer terminations and impact damage
    Jegley, Dawn C.
    1998, AIAA, Reston, VA, United States (35):
  • [40] Damage Tolerance of Pre-Stressed Composite Panels Under Impact Loads
    Johnson, Alastair F.
    Toso-Pentecote, Nathalie
    Schueler, Dominik
    APPLIED COMPOSITE MATERIALS, 2014, 21 (01) : 123 - 147