Micro-mechanical analysis of the in situ effect in polymer composite laminates

被引:131
作者
Arteiro, A. [1 ]
Catalanotti, G. [1 ]
Melro, A. R. [2 ]
Linde, P. [3 ]
Camanho, P. P. [1 ]
机构
[1] Univ Porto, Fac Engn, DEMec, P-4200465 Oporto, Portugal
[2] Univ Porto, INEGI, P-4200465 Oporto, Portugal
[3] AIRBUS Operat GmbH, D-21129 Hamburg, Germany
关键词
Laminates; In situ effect; Micro-mechanics; FEA; MATRIX CRACKING; GLASS/EPOXY COMPOSITES; NOTCHED RESPONSE; FAILURE CRITERIA; PART II; PLY; SIZE; PROPAGATION; PREDICTION; STRENGTH;
D O I
10.1016/j.compstruct.2014.06.014
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A micro-mechanical finite element model of a composite sublaminate is proposed to study the mechanical response of ultra-thin plies, consisting of a representative volume element of a 90 degrees thin lamina in-between two homogenised +/-theta degrees plies. Random fibre distributions, materially and statistically equivalent to real distributions, are analysed. A three-dimensional computational micro-mechanics framework, with a special focus on the elastic-plastic and damage constitutive behaviours of the matrix and on the response of the fibre-matrix interface, is used in the present analysis. Varying the 90 degrees ply thickness, it is possible to assess its effect on the mechanical response of laminated composites - the in situ effect. The proposed framework is able to accurately represent the micro-mechanical response of ultra-low grades, including (i) the mechanics of transverse cracking onset and propagation, (ii) the constraining effect observed in the laminae embedded in multidirectional laminates, (iii) the gradual, slow stress relaxation and progressive transverse cracking observed in very thin plies, and consequent increase of the crack density, (iv) the reduction in crack-opening displacement of the transverse cracks with ply thinness, (v) the formation of thin necks of matrix material around the regions where interfacial damage is more pronounced, and (vi) the in situ strengths. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:827 / 840
页数:14
相关论文
共 69 条
  • [61] A novel FEM model for biaxial non-crimp fabric composite materials under tension
    Tessitore, Nicola
    Riccio, Aniello
    [J]. COMPUTERS & STRUCTURES, 2006, 84 (19-20) : 1200 - 1207
  • [62] Random models versus periodic models for fibre reinforced composites
    Trias, D.
    Costa, J.
    Mayugo, J. A.
    Hurtado, J. E.
    [J]. COMPUTATIONAL MATERIALS SCIENCE, 2006, 38 (02) : 316 - 324
  • [63] Determination of the critical size of a statistical representative volume element (SRVE) for carbon reinforced polymers
    Trias, D.
    Costa, J.
    Turon, A.
    Hurtado, J. E.
    [J]. ACTA MATERIALIA, 2006, 54 (13) : 3471 - 3484
  • [64] Tsai S.W., 2008, Theory of composites design
  • [65] Transverse single-fibre test for interfacial debonding in composites .2. Modelling
    Varna, J
    Berglund, LA
    Ericson, ML
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1997, 28 (04) : 317 - 326
  • [66] Micromechanical modelling of the transverse damage behaviour in fibre reinforced composites
    Vaughan, T. J.
    McCarthy, C. T.
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2011, 71 (03) : 388 - 396
  • [67] Size effects in unnotched tensile strength of unidirectional and quasi-isotropic carbon/epoxy composites
    Wisnom, M. R.
    Khan, B.
    Hallett, S. R.
    [J]. COMPOSITE STRUCTURES, 2008, 84 (01) : 21 - 28
  • [68] Experimental characterization of strength and damage resistance properties of thin-ply carbon fiber/toughened epoxy laminates
    Yokozeki, Tomohiro
    Aoki, Yuichiro
    Ogasawara, Toshio
    [J]. COMPOSITE STRUCTURES, 2008, 82 (03) : 382 - 389
  • [69] Damage characterization in thin-ply composite laminates under out-of-plane transverse loadings
    Yokozeki, Tomohiro
    Kuroda, Akiko
    Yoshimura, Akinori
    Ogasawara, Toshio
    Aoki, Takahira
    [J]. COMPOSITE STRUCTURES, 2010, 93 (01) : 49 - 57