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Full Length Article | Open Access

Biaxial tensile behavior of CoCrFeNi high-entropy alloy under dynamic and proportional loadings

Haoyang LIa,bLiqiang GAOb,cLin QIa,bYajing FENGb,cJingyu WANGa,bYulong LIa,b,c,d( )Qifeng YUa
School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China
Shaanxi Key Laboratory of Impact Dynamics and Engineering Applications, Northwestern Polytechnical University, Xi’an 710072, China
School of Civil Aviation, Northwestern Polytechnical University, Suzhou 215699, China
NPU Yangzi River Delta Research Institute, Suzhou 215400, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

The dynamic failure behavior of CoCrFeNi High-Entropy Alloy (HEA) under plane biaxial stress was investigated in detail. The dynamic biaxial tensile tests were conducted using an Electromagnetic Biaxial Split Hopkinson Tensile Bar (EBSHTB) system. For comparison, the quasi-static uniaxial and biaxial tensile tests, as well as dynamic uniaxial tensile tests, were performed respectively. A cruciform specimen suitable for large plastic deformation was designed and employed in the experiments. The Finite Element Method (FEM) verified that the improved cruciform specimen could satisfy the basic requirements. The feasibility of the proposed specimen was further confirmed through loading tests. Finally, the quasi-static and dynamic yield loci of the HEA in the first quadrant of the principal stress space were plotted. The results indicate that the alloy exhibits obvious strain hardening effect and strain rate strengthening effect, the yield locus and plastic work contours can be accurately described by Hill’48 criterion.

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Chinese Journal of Aeronautics
Pages 475-489

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Cite this article:
LI H, GAO L, QI L, et al. Biaxial tensile behavior of CoCrFeNi high-entropy alloy under dynamic and proportional loadings. Chinese Journal of Aeronautics, 2024, 37(9): 475-489. https://doi.org/10.1016/j.cja.2024.06.003

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Received: 02 October 2023
Revised: 13 November 2023
Accepted: 14 December 2023
Published: 08 June 2024
© 2024 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/).