Effect of fibre architecture on tensile pull-off behaviour of 3D woven composite T-joints

Article

Yan, Shibo, Zeng, Xuesen and Long, Andrew. 2020. "Effect of fibre architecture on tensile pull-off behaviour of 3D woven composite T-joints." Composite Structures. 242, pp. 1-9. https://doi.org/10.1016/j.compstruct.2020.112194
Article Title

Effect of fibre architecture on tensile pull-off behaviour of 3D woven composite T-joints

ERA Journal ID3731
Article CategoryArticle
AuthorsYan, Shibo (Author), Zeng, Xuesen (Author) and Long, Andrew (Author)
Journal TitleComposite Structures
Journal Citation242, pp. 1-9
Article Number112194
Number of Pages9
Year2020
PublisherElsevier
Place of PublicationUnited Kingdom
ISSN0263-8223
1879-1085
Digital Object Identifier (DOI)https://doi.org/10.1016/j.compstruct.2020.112194
Web Address (URL)https://www.sciencedirect.com/science/article/pii/S0263822320300106
Abstract

3D woven composites are frequently employed due to their improved through-thickness properties and high damage tolerance compared with laminated composites. Due to the large design space for 3D weave patterns, an in-depth understanding of the relationship between the weave parameters and mechanical properties is essential for the design of these materials. This numerical study investigates the effect of fibre architecture on the mechanical performance of 3D woven composite T-joints under tensile pull-off loading. Six weave pattern variations, subjected to the same preform manufacturing constraint, are designed and numerically analysed, along with another two that have been manufactured and tested for validation previously. Results show a significant architecture dependence in the mechanical responses. Following the design of experiments on weave patterns, the complex architecture-dependant effect is decoupled by two independent variables, yarn path entanglement and yarn path crossover. The study also provides design recommendations for 3D woven T-joint reinforcements under tensile pull-off loading.

Keywords3D woven composites; T-joints; Fibre architecture; Mechanical properties
Contains Sensitive ContentDoes not contain sensitive content
ANZSRC Field of Research 2020400101. Aerospace materials
401706. Numerical modelling and mechanical characterisation
Byline AffiliationsCentre for Future Materials
Institution of OriginUniversity of Southern Queensland
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