Modelling cyclic shear deformation of fibre/epoxy layers in fibre metal laminates

被引：16
|
作者：
Alderliesten, Rene [1 ]
Campoli, Glanni [1 ]
Benedictus, Rinze [1 ]
机构：
[1] Delft Univ Technol, Fac Aerosp Engn, Struct & Mat Lab, NL-2600 GB Delft, Netherlands
来源：
COMPOSITES SCIENCE AND TECHNOLOGY | 2007年 / 67卷 / 11-12期
关键词：
C; crack; deformation; delamination; B; fatigue; C. fibre bridging;
D O I：
10.1016/j.compscitech.2006.12.011
中图分类号：
TB33 [复合材料];
学科分类号：
摘要：
Relations for a theoretical model were derived describing the shear deformation of uni-directional fibre/epoxy layers in Fibre Metal Laminates. The shear deformation is induced by the cyclic shear stresses at the interface that result from the cyclic load transfer from aluminium to the bridging fibre/epoxy layers during fatigue loading of the laminate. With the presented relations the crack opening contribution as result of shear deformation can be calculated. As the shear deformation is hard to measure experimentally, the theoretical model has been validated by comparing the model with finite element analysis. A good correlation has been obtained between the presented theoretical model and the FE-model representing the complex reality. (c) 2007 Elsevier Ltd. All rights reserved.
引用
收藏
页码：2545 / 2555
页数：11
相关论文
共 50 条
  • [1] Modelling Blast Response of Fibre Metal Laminates
    Guan, Z. W.
    Vo, T. P.
    Cantwel, W. J.
    PROCEEDINGS OF THE 4TH INTERNATIONAL CONFERENCE ON MECHANICAL ENGINEERING AND MECHANICS, 2011, : 64 - 69
  • [2] Tensile failure of fibre-metal-laminates made of titanium and carbon-fibre/epoxy laminates
    Sun, Jing
    Daliri, Ali
    Lu, Guoxing
    Ruan, Dong
    Lv, Yang
    MATERIALS & DESIGN, 2019, 183
  • [3] Analytical modelling and numerical simulation of the nonlinear deformation of hybrid fibre-metal laminates
    Wu, GC
    Yang, JM
    MODELLING AND SIMULATION IN MATERIALS SCIENCE AND ENGINEERING, 2005, 13 (03) : 413 - 425
  • [4] Flexural strength of aluminium carbon/epoxy fibre metal laminates
    Bellini, Costanzo
    Di Cocco, Vittorio
    Iacoviello, Francesco
    Sorrentino, Luca
    Material Design and Processing Communications, 2019, 1 (01):
  • [5] The modelling of impact loading on thermoplastic fibre-metal laminates
    Santiago, Rafael C.
    Cantwell, Wesley J.
    Jones, Norman
    Alves, Marcilio
    COMPOSITE STRUCTURES, 2018, 189 : 228 - 238
  • [6] Modelling and testing of fibre metal laminates and their constituent materials in fire
    Grigoriou, K.
    Mouritz, A. P.
    COMPOSITE STRUCTURES, 2018, 200 : 25 - 35
  • [7] Numerical Modelling of Fibre Metal Laminates Subjected to Blast Loading
    Guan, Z. W.
    Cantwell, W. J.
    ISCM II AND EPMESC XII, PTS 1 AND 2, 2010, 1233 : 101 - 106
  • [8] Reinforcement of CFRP joints with fibre metal laminates and additional adhesive layers
    dos Santos, D. G.
    Carbas, R. J. C.
    Marques, E. A. S.
    da Silva, L. F. M.
    COMPOSITES PART B-ENGINEERING, 2019, 165 : 386 - 396
  • [9] Interlaminar shear strength of fibre metal laminates after thermal cycles
    Jakubczak, Patryk
    Bienias, Jaroslaw
    Surowska, Barbara
    COMPOSITE STRUCTURES, 2018, 206 : 876 - 887
  • [10] Damage characterisation of fibre metal laminates under interlaminar shear load
    Hinz, Stephan
    Omoori, Toshihiro
    Hojo, Masaki
    Schulte, Karl
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2009, 40 (6-7) : 925 - 931
12345