Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/179438
Title: Failure mechanisms and process defects of 3D-printed continuous carbon fiber-reinforced composite circular honeycomb structures with different stacking directions
Authors: Zhang, Xin
Zheng, Xitao
Han, Yagang
Tian, Yuanyuan
Zhang, Di
Yan, Leilei
Keywords: Engineering
Issue Date: 2024
Source: Zhang, X., Zheng, X., Han, Y., Tian, Y., Zhang, D. & Yan, L. (2024). Failure mechanisms and process defects of 3D-printed continuous carbon fiber-reinforced composite circular honeycomb structures with different stacking directions. Aerospace Science and Technology, 148, 109075-. https://dx.doi.org/10.1016/j.ast.2024.109075
Journal: Aerospace Science and Technology
Abstract: 3D printing of continuous carbon fiber-reinforced composites relieves molds in composite manufacturing and gives flexibility to the design of lightweight and robust circular honeycomb structures. Nevertheless, how process defects affect the failure mechanisms of 3D-printed continuous carbon fiber-reinforced honeycomb structures remains undisclosed. To advance this research area, it requires a comprehensive investigation of the failure mechanisms and process defects of 3D-printed continuous carbon fiber-reinforced composite circular honeycomb structures (CCFRCCHSs), with particular attention to the influence of stacking orientations. In this study, 3D printing has been introduced to fabricate CCFRCCHSs using the identical composite material and geometry but different stacking orientations. Both in-plane and out-of-plane quasi-static compression experiments were carried out on these CCFRCCHSs. The mechanical properties and failure mechanisms were investigated through experimental analysis and cross-section observation, from which the microscopic voids and weak interfaces were identified as the dominating factors influencing the failure modes of CCFRCCHSs. This study provides insights into the association between process defects and failure mechanisms of 3D-printed CCFRCCHSs with different stacking directions, which offers guidance for the design of lightweight and robust composite circular honeycomb structures.
URI: https://hdl.handle.net/10356/179438
ISSN: 1270-9638
DOI: 10.1016/j.ast.2024.109075
Schools: School of Mechanical and Aerospace Engineering 
Rights: © 2024 Elsevier Masson SAS. All rights reserved.
Fulltext Permission: none
Fulltext Availability: No Fulltext
Appears in Collections:MAE Journal Articles

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