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author:

Zhao, Q. (Zhao, Q..) [1] | Tang, K. (Tang, K..) [2] | Wu, W. (Wu, W..) [3] | Li, Y. (Li, Y..) [4] | Deng, J. (Deng, J..) [5] | Chen, P. (Chen, P..) [6]

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Scopus

Abstract:

In order to establish a numerical analysis method for fatigue crack initiation and short crack propagation in polycrystalline steels, a microstructure model with cumulative fatigue damage was generated based on Roe-Siegmund cyclic cohesive zone model and Voronoi diagram method, and the mechanical properties of grains at the microscopic level were considered. Each grain was assigned a random local coordinate system and an anisotropic linear elastic constitutive. Finally, the effects of the microscopic defects such as pores and inclusions on the crack initiation path and life were studied. The results show that the method is consistent with the actual situation in the crack initiation path, and there are two fracture modes, transgranular and intergranular, with the latter being the dominant one. The crack initiation life range values in accordance with the normal distribution can be obtained, which is consistent with the experimental in the literature. The crack initiation path and the life of the crack initiation are changed. © 2025 Editorial Board of Mechanical Science and Technology for Aerospace Engineering. All rights reserved.

Keyword:

Cohesive element cyclic cohesive zone model metal fatigue fracture micro defects Voronoi

Community:

  • [ 1 ] [Zhao Q.]College of Civil Engineering, Fuzhou University, Fuzhou, 350116, China
  • [ 2 ] [Tang K.]College of Civil Engineering, Fuzhou University, Fuzhou, 350116, China
  • [ 3 ] [Wu W.]Fujian College Association Instrumental Analysis Center, Fuzhou University, Fuzhou, 350116, China
  • [ 4 ] [Li Y.]College of Civil Engineering, Fuzhou University, Fuzhou, 350116, China
  • [ 5 ] [Deng J.]College of Civil Engineering, Fuzhou University, Fuzhou, 350116, China
  • [ 6 ] [Chen P.]College of Civil Engineering, Fuzhou University, Fuzhou, 350116, China

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Source :

Mechanical Science and Technology for Aerospace Engineering

ISSN: 1003-8728

Year: 2025

Issue: 2

Volume: 44

Page: 361-372

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SCOPUS Cited Count:

ESI Highly Cited Papers on the List: 0 Unfold All

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Chinese Cited Count:

30 Days PV: 0

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