Simulation of interface damage in metal matrix composites under off-axis loading using cohesive zone model

被引:12
作者
Aghdam, M. M. [1 ]
Hosseini, S. M. A. [1 ]
Morsali, S. R. [1 ]
机构
[1] Amirkabir Univ Technol, Dept Mech Engn, Thermoelast Ctr Excellence, Tehran, Iran
关键词
Metal-matrix composites (MMCs); Finite element analysis (FEA); Residual stress; Interface failure; Off-axis loading; RESIDUAL-STRESSES; STRENGTH; MICROMECHANICS; FIBERS; ALLOY;
D O I
10.1016/j.commatsci.2015.05.030
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A finite element, micromechanical model is developed to predict the inelastic behavior of SiC/Ti composites subjected to off-axis loading using a three-dimensional representative volume element (RVE). The model includes the effects of manufacturing process thermal residual stresses together with interface damage and fiber coating. The cohesive zone model is used to consider the imperfect interface between the fiber and matrix. Introducing a unique failure criterion for various off-axis angles is the main novelty of this study. Apart from interface damage, plastic deformation of the matrix is also considered as another source of nonlinearity. Appropriate boundary conditions are imposed on the RVE to allow simultaneous application of a combined normal axial and transverse and axial shear loading plus thermal residual stresses. Results of the presented finite element model are compared with experimental data for stress-strain response, initiation of nonlinearity, and ultimate strength in various off-axis angles which show good agreement. Moreover, parametric studies are conducted to examine the effects of thermal residual stress and fiber volume fraction (FVF) on the mechanical response of the material. (C) 2015 Elsevier B.V. All rights reserved.
引用
收藏
页码:42 / 47
页数:6
相关论文
共 27 条
[11]   MODERN BORON AND SIC CVD FILAMENTS - A COMPARATIVE-STUDY [J].
LEPETITCORPS, Y ;
LAHAYE, M ;
PAILLER, R ;
NASLAIN, R .
COMPOSITES SCIENCE AND TECHNOLOGY, 1988, 32 (01) :31-55
[12]   Micromechanical modelling of SCS-6 fibre reinforced Ti-6Al-4V under transverse tension - Effect of fibre coating [J].
Li, DS ;
Wisnom, MR .
JOURNAL OF COMPOSITE MATERIALS, 1996, 30 (05) :561-588
[13]  
LI DS, 1994, COMPOS SCI TECHNOL, V51, P545
[14]   Fiber-matrix interfacial constitutive relations for metal matrix composites [J].
Lissenden, CJ .
COMPOSITES PART B-ENGINEERING, 1999, 30 (03) :267-278
[15]  
LISSENDEN CJ, 1996, ASTM INT W CONSHOHOC, P257, DOI DOI 10.1520/STP18227S
[16]   Study on longitudinal tensile properties of SiCf/Ti-6Al-4V composites with different interfacial shear strength [J].
Lou, J. H. ;
Yang, Y. Q. ;
Sun, Q. ;
Li, J. ;
Luo, X. .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2011, 529 :88-93
[17]   The analysis on transverse tensile behavior of SiC/Ti-6Al-4V composites by finite element method [J].
Lou, J. H. ;
Yang, Y. Q. ;
Luo, X. ;
Yuan, M. N. ;
Feng, G. H. .
MATERIALS & DESIGN, 2010, 31 (08) :3949-3953
[18]  
Naboulsi S, 2003, J COMPOS MATER, V37, P55, DOI 10.1106/002199803023468
[19]   A CONTINUUM MODEL FOR VOID NUCLEATION BY INCLUSION DEBONDING [J].
NEEDLEMAN, A .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1987, 54 (03) :525-531
[20]  
NIMMER RP, 1991, J COMPOS TECH RES, V13, P3, DOI 10.1520/CTR10068J