Thermo-mechanical coupling failure modeling of 3D four-directional braided composite I-beam under four-point flexure at room temperature,-50°C and 85°C

被引:0
|
作者
Li, Dong [1 ]
Xiong, Jun-Jiang [1 ]
Zhang, Hao-Ming [1 ]
机构
[1] Beihang Univ, Sch Transportat Sci & Engn, Dept Aircraft Airworthiness Engn, Beijing, Peoples R China
基金
中国国家自然科学基金;
关键词
Three-dimensional four-directional; braided composite; I-beam; four-point flexure; thermo-mechanical coupling; failure modeling; ELASTIC PROPERTIES; PREDICTION; MECHANISM; BEHAVIOR; TEMPERATURE; PARAMETERS; STRENGTH;
D O I
10.1080/15376494.2024.2402500
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper aims to experimentally and numerically probe thermo-mechanical coupling behaviors of 3D4D (three-dimensional four-directional) braided composite I-beam under four-point flexure. An improved algorithm based on thermo-mechanical coupling constitution model, and mixed failure criterion are devised for modeling thermo-mechanical coupling failure process of 3D4D braided composite I-beam under four-point flexure. Quasi-static four-point flexure tests are, respectively, performed on 3D4D braided composite I-beam at RT (room temperature), -50 degrees C and 85 degrees C, and mechanical behaviors and failure mechanisms are analyzed and discussed from experiment results. To validate the aforementioned model and algorithm, novel global-local FE (finite element) model is generated and integrated with new algorithm for modeling failure process of 3D4D braided composite I-beam under four-point flexure at three temperatures, and numerical predictions agree well with experimental findings, demonstrating the effective and rational use of the proposed model in the paper.
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页数:18
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