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Review | Publishing Language: Chinese | Open Access

Research progress in experimental and integrated calculations of high modulus magnesium based materials

Zhiqiang LI1Chuan SHUAI1Wei LIU1Hua HOU1,2Gaolong ZHANG2,3Yuhong ZHAO1,4( )
Collaborative Innovation Center of Ministry of Education and Shanxi Province for High-performance Al and Mg Alloy Materials,College of Materials Science and Engineering,North University of China,Taiyuan 030051,China
Taiyuan University of Science and Technology,Taiyuan 030024,China
Shanxi Shenzhou Aerospace Technology Co.,Ltd.,Jinzhong 030800,Shanxi,China
Beijing Advanced Innovation Center for Materials Genome Engineering,University of Science and Technology Beijing,Beijing 100083,China
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Abstract

Magnesium alloy is widely used in the aerospace field due to its low density, high specific strength, high damping and good thermal conductivity. However, its low elastic modulus limits its reliable application in large thin-walled components. Aiming at the problem to improve the modulus properties of magnesium-based materials, this paper briefly introduces the main factors affecting the modulus of the alloy, compares the advantages, disadvantages and application scope of relevant calculation models such as equal stress-strain model, rule of mixture, Halpin-Tsai model and two-phase composite model, summarizes the current situation and progress of the research on the modulus properties of magnesium-based materials, and reviews the two major ways of modulus improvement of magnesium-based materials and the mechanism of performance improvement. Based on the integrated computational material engineering, the integrated development strategy of high-strength and high-modulus magnesium-based materials for atomic-lattice scale analogy high-modulus aluminum alloy development and machine learning assisted optimization experimental design is proposed.

CLC number: V252.2;TB331 Document code: A

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Journal of Aeronautical Materials
Pages 43-64

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Cite this article:
LI Z, SHUAI C, LIU W, et al. Research progress in experimental and integrated calculations of high modulus magnesium based materials. Journal of Aeronautical Materials, 2024, 44(3): 43-64. https://doi.org/10.11868/j.issn.1005-5053.2023.000056

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Received: 20 April 2023
Revised: 31 August 2023
Published: 01 June 2024
© Journal of Aeronautical Materials 2024.

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