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Full Length Article | Open Access

Failure analysis of 3D woven composites under tension based on realistic model

Binbin ZHANGaGuangchang CHENbBing WANGcJingran GEa( )Mengran LIaZengfei LIUaJun LIANGa,d( )
Institute of Advanced Structure Technology, Beijing Institute of Technology, Beijing 100081, China
China Helicopter Research and Development Institute, Jingdezhen 333001, China
Center for Composite Materials and Structures, Harbin Institute of Technology, Harbin 150001, China
Beijing Key Laboratory of Lightweight Multi-functional Composite Materials and Structures, Beijing 100081, China

Peer review under responsibility of Editorial Committee of CJA

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Abstract

The failure behavior of the three-dimensional (3D) woven composites under tension are evaluated via experimentation and simulation. To accurately depict the intricate geometry of the woven composites, including the fluctuation of yarn paths, variations in cross-section, and resin distribution, the image-aided digital elements modeling approach is employed. Subsequently, to further assess both the tensile performance and damage response, a realistic voxel model is established with the integration of a well-suited progressive damage model. The obtained stress–strain curves align with the experimental results, and damage progression and underlying mechanisms involved are clearly revealed. Specifically, when subjected to warp tension, severe transverse damage and fiber bundle pull-out towards the warp yarns are observed within the curved section. Similarly, under weft loading, longitudinal damage is found to occur in the weft yarns, while the warp yarns suffer from transverse damage, leading to the formation of a smooth and brittle crack. Ultimately, the findings of this study hold potential to advance the engineering applications of the 3D woven composites.

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Chinese Journal of Aeronautics
Pages 242-253

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Cite this article:
ZHANG B, CHEN G, WANG B, et al. Failure analysis of 3D woven composites under tension based on realistic model. Chinese Journal of Aeronautics, 2024, 37(11): 242-253. https://doi.org/10.1016/j.cja.2024.07.032

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Received: 22 November 2023
Revised: 10 January 2024
Accepted: 23 March 2024
Published: 30 July 2024
© 2024 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/).