An interactive orthotropic non-local damage model for progressive failure analysis of composite laminates

被引:8
|
作者
Lu, X. [1 ,2 ]
Guo, X. M. [1 ]
机构
[1] Shanghai Univ, Shanghai Inst Appl Math & Mech, Sch Mech & Engn Sci, Shanghai Key Lab Mech Energy Engn, Shanghai 200444, Peoples R China
[2] Zhejiang Lab, Hangzhou 311100, Peoples R China
关键词
Laminates; Fracture; Computational modeling; Finite element analysis (FEA); FIBER-REINFORCED COMPOSITES; GRADIENT-ENHANCED DAMAGE; CONTINUUM DAMAGE; PART II; COHESIVE ELEMENT; TENSILE-STRENGTH; DELAMINATION; FRACTURE; PREDICTION; EMPHASIS;
D O I
10.1016/j.compstruct.2022.115841
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this study, the non-local continuum damage model is further developed for progressive failure analysis of laminated composites. Characterized by two internal length scales, an orthotropic non-local integral strategy is implemented to model the constrained matrix damage along fiber direction. The introduction of spatial averaging may avoid spurious strain localization and thus ensure the physically-meaningful energy dissipation during damage evolution process. Compared to standard damage descriptions, the pathological mesh sensitivity and mesh orientation bias are effectively alleviated, leading to objective and accurate solutions. Moreover, an interactive damage transfer scheme is proposed to capture the strong interaction between matrix cracking and interface delamination, so that faithful predictions on the complex failure mechanisms of composite laminates are guaranteed. Performance of the present model and its superiority over conventional methods are demonstrated through several numerical examples, including the typical tensile failure of notched and unnotched laminates.
引用
收藏
页数:12
相关论文
共 50 条
  • [21] Progressive damage model and analysis methodology for predicting the residual strength of composite laminates
    Harris, Charles E.
    Coats, Timothy W.
    Allen, David H.
    Lo, David C.
    Journal of Composites Technology and Research, 1997, 19 (01): : 3 - 9
  • [22] Isogeometric analysis for simulation of progressive damage in composite laminates
    Pigazzini, Marco S.
    Bazilevs, Yuri
    Ellison, Andrew
    Kim, Hyonny
    JOURNAL OF COMPOSITE MATERIALS, 2018, 52 (25) : 3471 - 3489
  • [23] Non-local orthotropic elastic shell model for vibration analysis of protein microtubules
    Taj, Muhammad
    Majeed, Arfan
    Hussain, Muzamal
    Naeem, Muhammad N.
    Safeer, Muhammad
    Ahmad, Manzoor
    Khan, Hidayat Ullah
    Tounsi, Abdelouahed
    COMPUTERS AND CONCRETE, 2020, 25 (03): : 245 - 253
  • [24] Non-local orthotropic damage-plastic model for 3D printed materials
    Linardi, Denis
    Monaldo, Elisabetta
    Marfia, Sonia
    INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2025, 310
  • [25] Failure analysis of anisotropic sheet-metals using a non-local plastic damage model
    Brunet, M
    Morestin, F
    Walter-Leberre, H
    JOURNAL OF MATERIALS PROCESSING TECHNOLOGY, 2005, 170 (1-2) : 457 - 470
  • [26] Progressive failure analysis of bolted joints in composite laminates
    Atas, A.
    Mohamed, G. F.
    Soutis, C.
    PLASTICS RUBBER AND COMPOSITES, 2012, 41 (4-5) : 209 - 214
  • [27] Progressive failure analysis of pin joints in composite laminates
    Evcil, Ali
    COMPUTATIONAL METHODS AND APPLIED COMPUTING, 2008, : 404 - 411
  • [28] Continuum Models for the Analysis of Progressive Failure in Composite Laminates
    Van Der Meer, F. P.
    Sluys, L. J.
    JOURNAL OF COMPOSITE MATERIALS, 2009, 43 (20) : 2131 - 2156
  • [29] A comprehensive study of the flexural behaviour and damage evolution of composite laminates using a progressive failure model
    El Idrissi, Hamza
    Seddouki, Abbass
    INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2023, 127 (7-8): : 3869 - 3890
  • [30] A comprehensive study of the flexural behaviour and damage evolution of composite laminates using a progressive failure model
    Hamza El Idrissi
    Abbass Seddouki
    The International Journal of Advanced Manufacturing Technology, 2023, 127 : 3869 - 3890