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Full Length Article | Open Access

A novel numerical simulation method for predicting compressive properties of 3D multiaxial braided composites considering various defects

Ruixin LEIa, Hao DOUa, Yan SUNa, Tao LIUa, Wei FANa,b( ), Chenyang SONGa, Shujuan WANGc, Yao LUa, Xue YANGd, Diansen LId
School of Textile Science and Engineering, Xi’an Polytechnic University, Xi’an 710048, China
Key Laboratory of Functional Textile Material and Product (Xi’an Polytechnic University), Ministry of Education, Xi’an 710048, China
School of Chemistry, Xi’an Jiaotong University, Xi’an 710049, China
Key Laboratory of Bio-Inspired Smart Interfacial Science and Technology, Ministry of Education, School of Chemistry, Beihang University, Beijing 100191, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

This paper reports a novel manufacturing process of preparing the Three-Dimensional Multiaxial Braided Composites (3DMBCs) and the effects of various defects generated in the manufacturing process on the compressive mechanical properties of 3DMBCs through the experimental and numerical methods. The five-step fabrication process of the 3D multiaxial braided preform was firstly introduced in detail. Then, the influences of various defects such as voids, waviness, and fiber breakage defects on the compressive properties of 3DMBCs were discussed. It is found that the fiber breakage defect and waviness defects were the two primary factors on the decrease of compressive properties of 3DMBCs. However, void defects in the resin and interface had little effect on the composites. When the fiber breakage defect content was 25% and the waviness was 7°, the composite compressive modulus decreased by 51%. The progressive damage process and failure mechanism of the composite under 90° compressive loading confirmed the validity of the numerical model by comparing with the experiments.

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Chinese Journal of Aeronautics
Pages 369-379

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Cite this article:
LEI R, DOU H, SUN Y, et al. A novel numerical simulation method for predicting compressive properties of 3D multiaxial braided composites considering various defects. Chinese Journal of Aeronautics, 2023, 36(9): 369-379. https://doi.org/10.1016/j.cja.2023.07.011

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Received: 20 July 2022
Revised: 14 August 2022
Accepted: 23 September 2022
Published: 19 July 2023
© 2023 Chinese Society of Aeronautics and Astronautics.

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