Finite element method analysis of fibre-metal laminates considering different approaches to material model

被引:11
|
作者
Smolnicki, Michal [1 ]
Stabla, Pawel [1 ]
机构
[1] Wroclaw Univ Sci & Technol, Dept Mech Mat & Engn, Wroclaw, Poland
来源
SN APPLIED SCIENCES | 2019年 / 1卷 / 05期
关键词
Fibre-metal laminates; FML; FEM; Composites; Laminates;
D O I
10.1007/s42452-019-0496-2
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
In this work, different approaches to fibre-metal laminates modelling are presented. Micromechanical, mesomechanical and macromechanical models are discussed. The application of these approaches for exemplary fibre-metal laminate made of aluminium and epoxy resin/glass fibre layers are shown. The classical laminate theory was used to obtain engineering constants for the macroscopic solid model and Puck criterion to obtain material data about epoxy resin/glass fibre layer. Various simulations using different simulation techniques were carried out in Simulia ABAQUS environment and results were compared with experimental data found in the literature. In conclusions, described approaches from the viewpoint of numerical simulation and experiment were evaluate. Research proves that mesoscopic (with distinguished layers of material) approach along with solid model gives the best results.
引用
收藏
页数:7
相关论文
共 50 条
  • [11] A Parametric Study of the Low-Impulse Blast Behaviour of Fibre-Metal Laminates Based on Different Aluminium Alloys
    Vo, Thuc
    Guan, Zhongwei
    Cantwell, Wesley
    Schleyer, Graham
    ACMTAA 2012: PROCEEDINGS OF THE SECOND INTERNATIONAL CONFERENCE ON ADVANCED COMPOSITE MATERIALS AND TECHNOLOGIES FOR AEROSPACE APPLICATIONS, 2012, : 69 - 74
  • [12] The Behaviour of Fibre-Metal Laminates under High Velocity Impact Loading with Different Stacking Sequences of Al Alloy
    Ramadhan, A. A.
    Abu Talib, A. R.
    Rafie, A. S. Mohd
    Zahari, R.
    AEROTECH IV: RECENT ADVANCES IN AEROSPACE TECHNOLOGIES, 2012, 225 : 213 - 218
  • [13] Finite element modelling of the impact response of fibre metal laminates under tension preloading
    Rathnasabapathy, M.
    Mouritz, A. P.
    Orifici, A. C.
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2022, 157
  • [14] A MATERIAL MODEL FOR THE FINITE-ELEMENT ANALYSIS OF METAL MATRIX COMPOSITES
    WU, JF
    SHEPHARD, MS
    DVORAK, GJ
    BAHEIELDIN, YA
    COMPOSITES SCIENCE AND TECHNOLOGY, 1989, 35 (04) : 347 - 366
  • [15] Inelastic finite element analysis of fibre-reinforced composite laminates with damage
    Chow, CL
    Yang, F
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 1998, 212 (08) : 717 - 729
  • [16] A finite element based statistical model for progressive tensile fibre failure in composite laminates
    Li, Xiangqian
    Hallett, Stephen R.
    Wisnom, Michael R.
    COMPOSITES PART B-ENGINEERING, 2013, 45 (01) : 433 - 439
  • [17] Investigation of the Contact Interface between Natural Fibre Metal Laminates under Tension Using Finite Element Analysis (FEA)
    Song, Chun Han
    Giasin, Khaled
    Saifullah, Abu
    Barouni, Antigoni
    POLYMERS, 2022, 14 (21)
  • [18] Finite Element Analysis Considering the Dipole Effect of Material Point
    Jiang, Qun
    Xia, Xiaozhou
    Zhang, Qing
    INTERNATIONAL CONFERENCE ON FRONTIERS OF ENERGY, ENVIRONMENTAL MATERIALS AND CIVIL ENGINEERING (FEEMCE 2013), 2013, : 655 - 664
  • [19] A finite element assessment of chip formation mechanisms in the machining of CFRP laminates with different fibre orientations
    Cepero-Mejias, F.
    Phadnis, V. A.
    Kerrigan, K.
    Curiel-Sosa, J. L.
    COMPOSITE STRUCTURES, 2021, 268
  • [20] Analysis of the contraction of the pelvic floor through the finite element method considering different pathologies
    da Roza, T. H.
    Parente, M. P. L.
    Natal Jorge, R. M.
    Mascarenhas, T.
    Loureiro, J.
    Duarte, S.
    TECHNOLOGY AND MEDICAL SCIENCES - TMSI 2010, 2011, : 39 - 42