A semi-analytical method for the determination of fracture toughness and bridging law in ELS test

被引:11
作者
Ding, Zhaohu [1 ]
Gong, Yu [1 ,2 ,3 ]
Wang, Ziming [1 ]
Zhang, Yongxiang [1 ,4 ]
Hu, Ning [1 ,5 ]
机构
[1] Chongqing Univ, Coll Aerosp Engn, Chongqing 400044, Peoples R China
[2] Chongqing Univ, State Key Lab Coal Mine Disaster Dynam & Control, Chongqing 400044, Peoples R China
[3] Jilin Univ, State Key Lab Automot Simulat & Control, Changchun 130022, Peoples R China
[4] Chongqing Univ, Chongqing Key Lab Heterogeneous Mat Mech, Chongqing 400044, Peoples R China
[5] Hebei Univ Technol, Sch Mech Engn, Tianjin 300401, Peoples R China
基金
中国国家自然科学基金;
关键词
Composite laminate; Fracture toughness; Bridging law; Mode -II delamination; R; -curve; II INTERLAMINAR FRACTURE; MODE-II; COHESIVE LAW; DELAMINATION GROWTH; BILINEAR APPROXIMATIONS; COMPOSITE; SIMULATION; CRITERION; CURVE; ENF;
D O I
10.1016/j.tafmec.2022.103712
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Fracture toughness and bridging law are necessary for characterizing the delamination behavior with the effect of fiber bridging. Accurate determination of them in a simple way is particularly important for the design of composite structures. The end-loaded split (ELS) method, which can obtain stable delamination growth, has been applied in the ISO 15,114 standard to measure the mode II fracture toughness. However, geometric nonlinearity and difficulty on the crack observation are unavoidable. To deal with those problems, a semi-analytical method is proposed in this study for determining the fracture toughness and the bridging law. Predictions from the semianalytical method are consistent with experimental results of CFRP and GFRP laminates. Furthermore, numerical modelling is performed based on a tri-linear cohesive zone model which integrates the determined bridging law. Numerical load-displacement responses have good agreements with the experimental ones, which illustrates the applicability and accuracy of the proposed method. The proposed method overcomes the problem of real-time monitoring of the crack growth length and the relative sliding displacement at the pre-crack tip, and considers the correction factors to solve the nonlinear problem caused by the large displacement, which is simple and efficient for practical application.
引用
收藏
页数:11
相关论文
共 66 条
  • [61] Efficiently determining the R-curve and bridging traction-separation relation of mode I delamination in a simple way
    Ye, Jinrui
    Gong, Yu
    Tao, Junan
    Cao, Tiancheng
    Zhao, Libin
    Zhang, Jianyu
    Hu, Ning
    [J]. COMPOSITE STRUCTURES, 2022, 288
  • [62] A novel four-linear cohesive law for the delamination simulation in composite DCB laminates
    Yin, Shihao
    Gong, Yu
    Li, Wangchang
    Zhao, Libin
    Zhang, Jianyu
    Hu, Ning
    [J]. COMPOSITES PART B-ENGINEERING, 2020, 180
  • [63] Measurement of mode II fracture toughness of wood by the end-notched flexure test
    Yoshihara, H
    Ohta, M
    [J]. JOURNAL OF WOOD SCIENCE, 2000, 46 (04) : 273 - 278
  • [64] Simulation of delamination growth in multidirectional laminates under mode I and mixed mode I/II loadings using cohesive elements
    Zhao, Libin
    Gong, Yu
    Zhang, Jianyu
    Chen, Yuli
    Fei, Binjun
    [J]. COMPOSITE STRUCTURES, 2014, 116 : 509 - 522
  • [65] Mode II delamination of a unidirectional carbon fiber/epoxy composite in four-point bend end-notched flexure tests
    Zile, E
    Tamuzs, V
    [J]. MECHANICS OF COMPOSITE MATERIALS, 2005, 41 (05) : 383 - 390
  • [66] Effect of interface angle on mode I delamination damage behavior of multidirectional fully isotropic laminates with the same global stiffness
    Zou, Luohuan
    Gong, Yu
    Tian, Dingli
    Zhao, Libin
    Zhang, Jianyu
    Hu, Ning
    [J]. THIN-WALLED STRUCTURES, 2023, 182