On the evaluation of in-plane elastic behaviour of woven fibre metal laminates under uniform loading

被引:0
|
作者
Sepiani, H. A. [1 ]
Afaghi-Khatibi, A. [1 ]
Mosavi, M. [1 ]
机构
[1] Univ Tehran, Dept Mech Engn, Tehran, Iran
关键词
woven fibre metal laminates; elastic large deformation; biaxial loading; finite-element analysis; EFFECTIVE CRACK-GROWTH; RESIDUAL STRENGTH; COMPOSITES; MODEL; PREDICTION; FABRICS;
D O I
10.1243/09544062JMES1303
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This article deals with the non-linear behaviour of woven fibre metal laminates (WFMLs). A theoretical micromechanical model has been proposed. for the plain-wave fabric-reinforced flexible composite with two surface-bonded metal layers under biaxial loading. The constitutive equations are derived through a strain energy approach and energy variation theorem based on the microstructure of composites. The modelling strategy starts with a geometrical description of the yarn and the unit cell and fibres are assumed to be in a sinusoidal shape. Meanwhile, a simple and conventional analytical technique is applied to predict the tensile properties of WFMLs. Stress-strain behaviour of such structure plates under uniform uniaxial loading are illustrated in figures. The proposed integrated micro mechanical model shows excellent agreement with the three-dimensional finite-element results. Finally, a parametric study is performed using the presented models to investigate the effect of thickness of metal layers on the elastic properties of the composite.
引用
收藏
页码:1027 / 1036
页数:10
相关论文
共 50 条
  • [31] Progressive failure analysis of carbon-fibre/epoxy composites laminates to study the effect of stitch densities under in-plane tensile loading
    Joshi, Prabij
    Kondo, Atsushi
    Watanabe, Naoyuki
    PLASTICS RUBBER AND COMPOSITES, 2017, 46 (04) : 147 - 154
  • [32] Fracture parameter evaluation of composite panels under in-plane loading
    Cai, G
    Yuan, FG
    COLLECTION OF THE 41ST AIAA/ASME/ASCE/AHS/ASC STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE AND EXHIBIT, VOL 1 PTS 1-3, 2000, : 1305 - 1315
  • [33] Evaluation of brick infill walls under in-plane and out-of-plane loading
    Bahreini, V.
    Mahdi, T.
    Najafizadeh, M. M.
    JOURNAL OF VIBROENGINEERING, 2017, 19 (01) : 394 - 408
  • [34] Buckling and vibrations of unsymmetric laminates resting on elastic foundations under in-plane and shear forces
    Aiello, MA
    Ombres, L
    COMPOSITE STRUCTURES, 1999, 44 (01) : 31 - 41
  • [35] 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
  • [36] Adhesively bonded glass-metal facade elements with composite structural behaviour under in-plane and out-of-plane loading
    Silvestru, Vlad Alexandru
    Kolany, Georg
    Freytag, Bernhard
    Schneider, Jens
    Englhardt, Oliver
    ENGINEERING STRUCTURES, 2019, 200
  • [37] Behaviour of basalt fibre reinforced polymer strengthened timber laminates under tensile loading
    Fernando, D.
    Frangi, A.
    Kobel, P.
    ENGINEERING STRUCTURES, 2016, 117 : 437 - 456
  • [38] Interfacial cracks between piezoelectric and elastic materials under in-plane electric loading
    Liu, M
    Hsia, KJ
    JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 2003, 51 (05) : 921 - 944
  • [39] Eccentric low-velocity impact on fiber-metal laminates under in-plane loading using unified zigzag theory
    Ghalami-Choobar, Mehran
    Liaghat, Gholamhossein
    Sadighi, Mojtaba
    Ahmadi, Hamed
    COMPOSITE STRUCTURES, 2018, 201 : 315 - 325
  • [40] Harmonic holes with surface tension in an elastic plane under uniform remote loading
    Dai, Ming
    Schiavone, Peter
    Gao, Cun-Fa
    MATHEMATICS AND MECHANICS OF SOLIDS, 2017, 22 (09) : 1806 - 1812