Research on fatigue crack propagation of a T-joint based on XFEM and TSA

被引:5
作者
Chen, Daoyun [1 ]
Li, Guangquan [2 ]
Wang, Yan [2 ]
Xiao, Qian [1 ]
机构
[1] East China Jiaotong Univ, Key Lab Conveyance & Equipment, Minist Educ, Nanchang 330013, Jiangxi, Peoples R China
[2] CRRC Qingdao Sifang Co Ltd, Tech Ctr, Qingdao 266111, Shandong, Peoples R China
基金
中国国家自然科学基金;
关键词
Fatigue crack propagation; Extended finite element method; Thermoelastic stress analysis; Stress intensity factor; Crack length detection; DIGITAL IMAGE CORRELATION; FINITE-ELEMENT-METHOD; NUMERICAL-SIMULATION; GROWTH SIMULATIONS; STRESS-ANALYSIS; BEHAVIOR; THERMOELASTICITY; REFINEMENT; TIP;
D O I
10.1016/j.engfracmech.2019.106707
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The extended finite element method (XFEM) and thermoelastic stress analysis (TSA) are employed to study crack propagation of a T-joint during fatigue testing. The test results of a non-welded T-shaped plate and a welded T-shaped plate are presented in the paper. The theory of XFEM is analysed, and finite element (FE) simulations are conducted to obtain the crack propagation results. The theory of TSA is analysed, and TSA tests are conducted. The temperature change distribution maps, average temperature distribution maps and phase distribution maps of the welded and non-welded specimens in several typical crack propagation stages are presented. The stress intensity factor (SIF) values are evaluated from the TSA maps by regression analysis. The Canny algorithm is employed to detect the crack length based on the temperature change maps of the TSA results. The simulation and experimental results of the XFEM and TSA are compared and summarized.
引用
收藏
页数:16
相关论文
共 54 条
  • [1] A simple heat diffusion model to avoid singularity in estimating a crack length using sonic infrared inspection technology
    Abu-Nabah, Bassam A.
    Al-Said, Samer M.
    Gouia-Zarrad, Rim
    [J]. SENSORS AND ACTUATORS A-PHYSICAL, 2019, 293 : 77 - 86
  • [2] Automatic procedure for evaluating the Paris Law of martensitic and austenitic stainless steels by means of thermal methods
    Ancona, F.
    Palumbo, D.
    De Finis, R.
    Demelio, G. P.
    Galietti, U.
    [J]. ENGINEERING FRACTURE MECHANICS, 2016, 163 : 206 - 219
  • [3] [Anonymous], ANSYS HELP REL 17 00
  • [4] [Anonymous], SIMULATION FATIGUE C
  • [5] Data-rich characterisation of damage propagation in composite materials
    Battams, G. P.
    Dulieu-Barton, J. M.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2016, 91 : 420 - 435
  • [6] Belytschko T, 1999, INT J NUMER METH ENG, V45, P601, DOI 10.1002/(SICI)1097-0207(19990620)45:5<601::AID-NME598>3.0.CO
  • [7] 2-S
  • [8] Fatigue crack growth simulations of interfacial cracks in bi-layered FGMs using XFEM
    Bhattacharya, S.
    Singh, I. V.
    Mishra, B. K.
    Bui, T. Q.
    [J]. COMPUTATIONAL MECHANICS, 2013, 52 (04) : 799 - 814
  • [9] Efficiency of crack detection based on damping characteristics
    Bovsunovsky, A. P.
    [J]. ENGINEERING FRACTURE MECHANICS, 2019, 214 : 464 - 473
  • [10] Thermoelasticity for the evaluation of fatigue behavior of 7005/Al2O3/10p metal matrix composite sheets joined by FSW
    Cavaliere, P.
    Rossi, G. L.
    Di Sante, R.
    Moretti, M.
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2008, 30 (01) : 198 - 206