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Open Access

An integrated preforming-performance model for high-fidelity performance analysis of cured woven composite part with non-orthogonal yarn angles

Biao LIANGaSasa GAObWeizhao ZHANGc( )
School of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710072, China
College of Mechanical & Electrical Engineering, Shaanxi University of Science & Technology, Xi’an 710021, China
Department of Mechanical and Automation Engineering, The Chinese University of Hong Kong, Hong Kong, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Preforming process would change yarn angle and yarn orientation, its influence on the material properties and material orientations needs to be considered in the performance analysis. However, most current performance models fail to account for the preforming effect. An integrated performance model accounting for the impact of preforming has been developed. In this integrated model, part geometry, yarn angle and orientation after preforming of multiple prepreg layers are predicted by Finite Element Analysis (FEA) using a non-orthogonal constitutive law. Experiments were conducted to validate the preforming simulation for a single dome composites structure made by two prepreg layers with different initial fiber orientations. Performance analysis until failure was then conducted for the single dome structure to validate the integrated performance model. Comparison between simulation and experiment shows that not only the failure mode and failure zone, but also the force-displacement curve during compression process are captured correctly by the performance model, demonstrating the effectiveness of the newly proposed model in accounting for the impact of preforming process.

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Chinese Journal of Aeronautics
Pages 367-378

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Cite this article:
LIANG B, GAO S, ZHANG W. An integrated preforming-performance model for high-fidelity performance analysis of cured woven composite part with non-orthogonal yarn angles. Chinese Journal of Aeronautics, 2022, 35(6): 367-378. https://doi.org/10.1016/j.cja.2021.09.019

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Received: 03 February 2021
Revised: 28 February 2021
Accepted: 24 April 2021
Published: 26 October 2021
© 2021 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/).