Abstract

Multiroute yield experiments were carried out on extruded ZK60 magnesium alloy samples under 200 °C and strain rate of 10−2 s−1 by a thermomechanical simulator. A hypoelastoplastic large deformation constitutive relationship was employed to simulate large deformation yield subjected to uniaxial loading, biaxial loading, loading-reverse loading, and orthogonal loading in the finite element (FE) software with user subroutine. The results showed the following: (1) As the accumulative plastic strain increased, the convex yield surface in the 2D stress space gradually expanded or shrank, rotated, and distorted from the approximate ellipse at low accumulative plastic strain. At the same accumulative plastic strain, uniaxial tensile or compressive yield values along different directions were not the same. In addition, the tensile yield value differed considerably from the compressive one. The large deformation yield of ZK60 magnesium alloy showed significant anisotropy, tension-compression strength difference, and evolution effect. (2) FE simulations based on the hypoelastoplastic constitutive relationship could accurately capture the strongly evolving asymmetric yield behavior under complex loading routes. The stress-strain relationships and hardening rates were in better accordance with the experimental results and reflected the yield behavior more realistically compared to simulations without the evolution effect or with traditional linear interpolation. Deformation at low temperature and high strain rate is important to save process costs and improve processing efficiency, but it may cause evolving asymmetric yield during large deformation. It is believed that the simulation approach used herein is reliable for the prediction and optimization of severe plastic deformation processes of hexagonal close-packed (HCP) alloys.

Highlights

  • Due to low density, high specific strength, good biocompatibility, and abundant reserves [1,2,3], magnesium and its alloys have attracted widespread attention for use in vehicles, aerospace, military equipment, intelligent technology, and medical devices [4,5,6,7].As a typical lightweight hexagonal close-packed (HCP) material, magnesium alloys are praised as the most promising metal material in the 21st century [8]

  • Developing low-cost and high-efficiency severe plastic deformation processes for plainified alloys is an effective way to better promote the application of magnesium in various industrial fields

  • The aims of the current study were to (1) reveal the significant yield anisotropy, strength difference effect (SDE), and yield surface evolution behavior of plain ZK60 Mg alloy under low temperature and high strain rate and (2) validate the reliability of the approach used in the current study for the simulation of evolving large deformation asymmetric yield of Mg alloys

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Summary

Introduction

High specific strength, good biocompatibility, and abundant reserves [1,2,3], magnesium and its alloys have attracted widespread attention for use in vehicles, aerospace, military equipment, intelligent technology, and medical devices [4,5,6,7]. At low temperature, high strain rate, and large deformation, magnesium alloys may exhibit strongly evolving yield anisotropy and tension-compression strength difference effect (SDE), making it difficult to predict and control the product profile and texture. To accurately capture the strongly evolving yield anisotropy and SDE at low temperature, high strain rate, and large deformation, it is necessary to develop a reasonable asymmetric yield function, large deformation constitutive relationship, and yield surface evolution description. The aims of the current study were to (1) reveal the significant yield anisotropy, SDE, and yield surface evolution behavior of plain ZK60 Mg alloy under low temperature and high strain rate and (2) validate the reliability of the approach used in the current study for the simulation of evolving large deformation asymmetric yield of Mg alloys

Materials
Electron Backscatter Diffraction Characterization
Compression and Tension Tests
FE Algorithm
Displacement
3.Results
Uniaxial Loading
Biaxial
Finite
Loading-Reverse Loading
Orthogonal Loading
Orthogonal
Conclusions
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