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

被引:0
|
作者
Li, Haoyang [1 ,2 ]
Gao, Liqiang [2 ,3 ]
Qi, Lin [1 ,2 ]
Feng, Yajing [2 ,3 ]
Wang, Jingyu [1 ,2 ]
Li, Yulong [1 ,2 ,3 ,4 ]
Yu, Qifeng [1 ]
机构
[1] Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China
[2] Northwestern Polytech Univ, Shaanxi Key Lab Impact Dynam & Engn Applicat, Xian 710072, Peoples R China
[3] Northwestern Polytech Univ, Sch Civil Aviat, Suzhou 215699, Peoples R China
[4] NPU Yangzi River Delta Res Inst, Suzhou 215400, Peoples R China
基金
中国国家自然科学基金;
关键词
High-entropy alloys; Biaxial tensile test; Cruciform specimen; Electromagnetic split Hop- kinson bar; Digital image correlation;
D O I
10.1016/j.cja.2024.06.003
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
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. (c) 2024 Production and hosting by Elsevier Ltd. on behalf of Chinese Society of Aeronautics and Astronautics. This is an open access article under the CC BY-NC-ND license .
引用
收藏
页码:475 / 489
页数:15
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