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Author:

Li, Dao-Hang (Li, Dao-Hang.) | Shang, De-Guang (Shang, De-Guang.) (Scholars:尚德广) | Chen, Hong (Chen, Hong.) | Cong, Ling-Hua (Cong, Ling-Hua.) | Wang, Jin-Jie (Wang, Jin-Jie.) | Zhou, Xue-Peng (Zhou, Xue-Peng.) | Zhao, Yi-Ru (Zhao, Yi-Ru.) | Li, Wei (Li, Wei.) | Mao, Zheng-Yu (Mao, Zheng-Yu.)

Indexed by:

EI Scopus SCIE

Abstract:

In this paper, the experimental investigation was carried out on the TC4 titanium alloy to understand the cyclic deformation behavior and fatigue damage mechanism of materials under multiaxial thermo-mechanical loading. The results showed that the fast cracking mode of the material may be activated by the combined action of high temperature, tensile stress and shear stress, inducing a fast degradation in the axial mechanical properties of the material, which results in a drastic decrease in the failure life of the material. Moreover, it is also found that the non-proportional additional hardening and the tensile mean stress can increase the fatigue and oxidation damages of the material, and the material damage behavior is temperature dependent and time dependent. It should be pointed out that the damage mechanisms identified in this paper can reasonably explain the life law under uniaxial isothermal fatigue loading with and without dwell time, uniaxial and multiaxial thermomechanical fatigue loadings.

Keyword:

Multiaxial thermo-mechanical fatigue Deformation behavior Fatigue-oxidation Damage mechanism Titanium alloy

Author Community:

  • [ 1 ] [Li, Dao-Hang]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 2 ] [Shang, De-Guang]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 3 ] [Wang, Jin-Jie]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 4 ] [Zhou, Xue-Peng]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 5 ] [Zhao, Yi-Ru]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 6 ] [Li, Wei]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 7 ] [Mao, Zheng-Yu]Beijing Univ Technol, Fac Mat & Mfg, Beijing 100124, Peoples R China
  • [ 8 ] [Chen, Hong]Aircraft Strength Res Inst China, Xian 710065, Peoples R China
  • [ 9 ] [Cong, Ling-Hua]Aircraft Strength Res Inst China, Xian 710065, Peoples R China

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Source :

THEORETICAL AND APPLIED FRACTURE MECHANICS

ISSN: 0167-8442

Year: 2022

Volume: 121

5 . 3

JCR@2022

5 . 3 0 0

JCR@2022

ESI Discipline: ENGINEERING;

ESI HC Threshold:49

JCR Journal Grade:1

CAS Journal Grade:2

Cited Count:

WoS CC Cited Count: 8

SCOPUS Cited Count: 10

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 7

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