A digital twin approach toward unlocking elasto-plastic fatigue crack growth rates under negative load ratios

被引:1
|
作者
Cheok, Evan Wei Wen [1 ]
Qian, Xudong [1 ]
Quek, Ser Tong [1 ]
Si, Michael Boon Ing [1 ]
机构
[1] Natl Univ Singapore, Dept Civil & Environm Engn, Singapore 117576, Singapore
关键词
Digital twin; Data -driven approach; Cracks; Elasto-plastic fatigue crack growth; Variable amplitude loading; HIGH-STRENGTH STEEL; PROPAGATION; PREDICTION;
D O I
10.1016/j.engfracmech.2024.110034
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper introduces a novel digital twin solution for unlocking the elasto-plastic fatigue crack growth within an S550 steel under negative load ratios. The digital twin transforms solely strain data from a strain-interfaced welded plate joint specimen to the load-displacement curve to compute cyclic J-integral values using the eta approach, eliminating the need for load and displacement measurements. The accurate computation of the elasto-plastic Delta J effectively extends the fatigue crack growth relationship derived from standard fracture specimens. The extended fatigue crack growth relationship accurately predicts the fatigue life of specimens under separate step-up and step-down variable amplitude loading regimes.
引用
收藏
页数:17
相关论文
共 33 条
  • [1] Role of elasto-plastic analysis under cyclic loading in fatigue crack growth studies
    Dattaguru, B.
    Sadhana - Academy Proceedings in Engineering Sciences, 1996, 21 (pt 5): : 577 - 595
  • [2] Fatigue crack growth in Ti-6242 under elasto-plastic loading conditions
    Hornqvist, Magnus
    Mansson, Tomas
    FATIGUE 2010, 2010, 2 (01): : 223 - 229
  • [3] Role of elasto-plastic analysis under cyclic loading in fatigue crack growth studies
    Dattaguru, B
    SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES, 1996, 21 : 577 - 595
  • [4] Experimental study on fatigue crack growth for engineering small cracks under elasto-plastic condition
    Minzhong, Zheng
    Xuezhou, Nie
    Xiaoguang, Liu
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 1991, 12 (02):
  • [5] Prediction of fatigue crack growth under constant amplitude loading and a single overload based on elasto-plastic crack tip stresses and strains
    Noroozi, A. H.
    Glinka, G.
    Lambert, S.
    ENGINEERING FRACTURE MECHANICS, 2008, 75 (02) : 188 - 206
  • [6] Elasto-plastic fatigue crack growth analysis of plane problems in the presence of flaws using XFEM
    Sachin KUMAR
    A.S.SHEDBALE
    I.V.SINGH
    B.K.MISHRA
    Frontiers of Structural and Civil Engineering, 2015, 9 (04) : 420 - 440
  • [7] Elasto-plastic fatigue crack growth analysis of plane problems in the presence of flaws using XFEM
    Sachin Kumar
    A. S. Shedbale
    I. V. Singh
    B. K. Mishra
    Frontiers of Structural and Civil Engineering, 2015, 9 : 420 - 440
  • [8] Elasto-plastic fatigue crack growth analysis of plane problems in the presence of flaws using XFEM
    Kumar, Sachin
    Shedbale, A. S.
    Singh, I. V.
    Mishra, B. K.
    FRONTIERS OF STRUCTURAL AND CIVIL ENGINEERING, 2015, 9 (04) : 420 - 440
  • [9] Effect of compressive load and crack closure on fatigue crack growth of commercial pure titanium at negative load ratios
    Zhang, Peng
    Zhou, Chang-yu
    Li, Jian
    Miao, Xin-ting
    He, Xiao-hua
    ENGINEERING FRACTURE MECHANICS, 2019, 219
  • [10] Analysis of delamination fatigue growth for delaminated piezoelectric elasto-plastic laminated beams under hygrothermal conditions
    Li, Y. L.
    Fu, Y. M.
    Mao, Y. Q.
    COMPOSITE STRUCTURES, 2011, 93 (02) : 889 - 901