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Open Access

Residual stress indentation model based on material equivalence

Xiaokun LIUaLixun CAIa( )Hui CHENb
Applied Mechanics and Structure Safety Key Laboratory of Sichuan Province, School of Mechanics and Engineering, Southwest Jiaotong University, Chengdu 610031, China
School of Civil Engineering, Changsha University of Science & Technology, Changsha 410114, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

A novel residual stress indentation model for conical indentation loading is proposed to describe the relationship between the residual stress, material constitutive parameters, load, and displacement for materials with a uniaxial constitutive relationship that obeys Hollomon’s power law (H-law). The novel model was established based on the principle that the equivalent material without residual stress corresponds to the original material with residual stress, conical indentation theoretical model based on energy density equivalence, and an assumed power-law relationship between the dimensionless residual stress and relative difference of the yield stresses of the equivalent material and original material. Sixty imaginary H-law materials with ten equibiaxial and ten uniaxial residual stresses were investigated by Finite Element Analysis (FEA). The residual stresses predicted by the novel model from the indentation load–displacement curves simulated for the imaginary materials are in close agreement with those applied by the FEA. Finally, indentation tests for Cr12MoV steel, 45 steel, and 6061-T6511 aluminum alloy were carried out on their specimens without residual stress and their bending specimens with equibiaxial and uniaxial residual stresses. The residual stresses predicted by the novel model according to the indentation load–displacement test curves are in good agreement with those applied by the tests.

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Chinese Journal of Aeronautics
Pages 304-313

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Cite this article:
LIU X, CAI L, CHEN H. Residual stress indentation model based on material equivalence. Chinese Journal of Aeronautics, 2022, 35(8): 304-313. https://doi.org/10.1016/j.cja.2022.01.025

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Received: 25 March 2021
Revised: 06 May 2021
Accepted: 02 August 2021
Published: 03 February 2022
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).