Effects of different joint wall lengths on in-plane compression properties of 3D braided jute/epoxy composite honeycombs

Journal Article (2023)
Author(s)

Li Qian-Qian (Donghua University)

Yasmine Mosleh (TU Delft - Bio-based Structures & Materials)

R.C. Alderiesten (TU Delft - Structural Integrity & Composites)

Zhang Hong-Hua (Donghua University)

Li Wei (Ministry of Education, Shanghai, Donghua University)

Research Group
Bio-based Structures & Materials
Copyright
© 2023 Li Qian-Qian, Yasmine Mosleh, R.C. Alderliesten, Zhang Hong-Hua, Li Wei
DOI related publication
https://doi.org/10.1177/07316844231167898
More Info
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Publication Year
2023
Language
English
Copyright
© 2023 Li Qian-Qian, Yasmine Mosleh, R.C. Alderliesten, Zhang Hong-Hua, Li Wei
Research Group
Bio-based Structures & Materials
Bibliographical Note
Green Open Access added to TU Delft Institutional Repository ‘You share, we take care!’ – Taverne project https://www.openaccess.nl/en/you-share-we-take-care Otherwise as indicated in the copyright section: the publisher is the copyright holder of this work and the author uses the Dutch legislation to make this work public. @en
Issue number
9-10
Volume number
43
Pages (from-to)
547-564
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Abstract

To comply with the trend in the development of engineering materials towards lightweight, high strength, eco-friendly, sustainable, and multi-functional, a three-dimensional braided integrated composite honeycomb is designed. The effects of geometrical parameters particularly joint wall lengths on the in-plane mechanical behavior of the honeycombs were investigated. The results show that the in-plane mechanical properties are related to the number of cell walls, and the angle between the cell wall and the loading direction. Increasing the number of cell rows to double and triple at similar areal density lead to an improvement of the maximum load up to 2.5, and 3.8 times, respectively. Similarly, the total absorbed strain energy increased up to 2.6 and 5.9 times, respectively. The displacement at the maximum load is increased by 1.6 and 2.7 times as a result of increasing the cell row number. The total absorbed strain energy increased to 1.7 and 1.3 times, respectively. The failure angle of the 3D braided composite honeycomb is about 4°–7°. This investigation presents the geometrical factors of a 3D braided composite honeycomb can be further designed and optimized, but it also provides a reference for the development and design of a new composite honeycomb.

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