An Analysis of Tensile and Compressive Properties of Carbon Fiber High-Entropy Alloy Composite Laminates

被引:1
|
作者
Guo, Z. X. [1 ,4 ]
Shi, H. L. [1 ]
Ma, S. G. [1 ,3 ]
Cui, J. J. [1 ]
Chai, G. B. [2 ]
Li, Y. C. [5 ]
机构
[1] Taiyuan Univ Technol, Inst Appl Mech, Coll Mech & Vehicle Engn, Taiyuan 030024, Peoples R China
[2] Nanyang Technol Univ, Sch Mech & Aerosp Engn, 50 Nanyang Ave, Singapore 639798, Singapore
[3] Beijing Inst Technol, State Key Lab Explos Sci & Technol, Beijing 100081, Peoples R China
[4] Taiyuan Univ Technol, Inst Appl Mech, Shanxi Key Lab Mat Strength & Struct Impact, Taiyuan 030024, Peoples R China
[5] Taiyuan Univ Technol, Natl Demonstrat Ctr Expt Mech Educ, Taiyuan 030024, Peoples R China
基金
中国国家自然科学基金;
关键词
carbon fiber; high-entropy alloy; composite laminate; tensile and compression tests; mechanical properties; LOW-VELOCITY IMPACT; BEHAVIOR; FAILURE;
D O I
10.1007/s11029-023-10162-2
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Tensile tests were carried out on carbon fiber high-entropy alloy, carbon fiber aluminum alloy, carbon fiber titanium alloy, and carbon fiber-reinforced composite laminates. Their mechanical properties were investigated at the tensile strain rates of 3 center dot 10-3, 1 center dot 10-3, and 1 center dot 10-4 s-1. Compression tests on carbon fiber high entropy alloy (HEA) and carbon fiber-reinforced composite laminates were carried out at the strain rates of 3 center dot 10-3 and 1 center dot 10-3 s-1, respectively. Results showed that the carbon fiber high-entropy alloy composite laminate was more elastic than the carbon fiber-reinforced composite laminate at the strain rates of 3 center dot 10-3, 1 center dot 10-1, and 1 center dot 10-4 s-1. Their strength increased by 27, 16, and 10%, and the breaking strength by 18, 12, and 14%, respectively. Compared with the carbon fiber-reinforced composite laminate, the compressive strength of the carbon fiber HEA composite laminate increased by 44 and 29% at the compressive strain rates of 3 center dot 10-3 and 1 center dot 10-3s-1, respectively.
引用
收藏
页码:1147 / 1156
页数:10
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