A novel material degradation model for unidirectional CFRP composites

被引:37
作者
Zhao, Libin [1 ]
Li, Yang [1 ]
Zhang, Jianyu [2 ]
Zhou, Longwei [1 ]
Hu, Ning [2 ]
机构
[1] Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China
[2] Chongqing Univ, Coll Aerosp Engn, Chongqing 400044, Peoples R China
基金
美国国家科学基金会;
关键词
Laminates; Mechanical properties; Damage mechanics; Finite element analysis (FEA); Joints/joining; PROGRESSIVE FAILURE ANALYSIS; FIBER-REINFORCED COMPOSITES; FINITE-ELEMENT-ANALYSIS; MECHANICALLY FASTENED JOINTS; INDUCED LAMINATE FAILURE; DAMAGE MODEL; COMPRESSIVE FAILURE; BOLTED JOINTS; PI-JOINT; PART II;
D O I
10.1016/j.compositesb.2017.09.038
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A novel material degradation model (MDM), which is an essential component of progressive damage models for failure analysis of composite structures, is proposed based on the representative volume element (RVE) method. In this model, a material degradation rule accounting for seven failure modes in a modified Hashin-type failure criterion is proposed. This rule determines the mechanical parameters that are degraded when a failure occurs. The degradation factors of these parameters are calculated from the RVE models for perfect and damaged materials corresponding to the seven failure modes, which are based on the fundamental properties of transverse isotropic fibers and isotropic matrix. To verify the proposed method, the calculated MDMs are used in the progressive failure analyses of open-hole laminates made of three types of CFRP composites under tensile and compressive loadings. Furthermore, the failure analyses of four kinds of double-lap single-bolted joint structures with various layups and geometry dimensions are also conducted under tensile loading. The numerical predictions of failure loads, failure patterns and load-displacement curves are compared to the experimental results. Good agreement between the model predictions and the experimental results demonstrates the effectiveness of the proposed MDM for the progressive damage analyses of open-hole laminates and composite bolted joints. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:84 / 94
页数:11
相关论文
共 77 条
  • [1] [Anonymous], 2004, ASTM D6484-04
  • [2] [Anonymous], 2001, D5961M01 ASTM
  • [3] [Anonymous], 2002, D576602 ASTM
  • [4] Micro-mechanical analysis of the effect of ply thickness on the transverse compressive strength of polymer composites
    Arteiro, A.
    Catalanotti, G.
    Melro, A. R.
    Linde, P.
    Camanho, P. P.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2015, 79 : 127 - 137
  • [5] Experimental and analytical study on fiber-kinking failure mode of laminated composites
    Ataabadi, A. Kabiri
    Hosseini-Toudeshky, H.
    Rad, S. Ziaei
    [J]. COMPOSITES PART B-ENGINEERING, 2014, 61 : 84 - 93
  • [6] Progressive damage modelling of hybrid RTM-made composite Π-joint under four-point flexure using mixed failure criteria
    Bai, J. B.
    Shenoi, R. A.
    Yun, X. Y.
    Xiong, J. J.
    [J]. COMPOSITE STRUCTURES, 2017, 159 : 327 - 334
  • [7] High-fidelity micro-scale modeling of the thermo-visco-plastic behavior of carbon fiber polymer matrix composites
    Bai, Xiaoming
    Bessa, Miguel A.
    Melro, Antonio R.
    Camanho, Pedro P.
    Guo, Licheng
    Liu, Wing K.
    [J]. COMPOSITE STRUCTURES, 2015, 134 : 132 - 141
  • [8] Progressive failure analysis of open-hole composite hoops under radial loading
    Bai, Yujie
    Zhang, Xiao-Zhang
    [J]. COMPOSITES PART B-ENGINEERING, 2016, 97 : 336 - 343
  • [9] Determination of material parameters for Abaqus progressive damage analysis of E-glass epoxy laminates
    Barbero, E. J.
    Cosso, F. A.
    Roman, R.
    Weadon, T. L.
    [J]. COMPOSITES PART B-ENGINEERING, 2013, 46 : 211 - 220
  • [10] Compressive failure of fiber composites under multi-axial loading
    Basu, S
    Waas, AM
    Ambur, DR
    [J]. JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 2006, 54 (03) : 611 - 634