Abstract
Composite sandwich structures are widely used in transport and energy applications because of their excellent specific strength and fatigue damage resistance. However, the mechanical properties of the joint area rely on the structural design. This paper proposes a novel carbon fiber-reinforced polymer sandwich joint in the context of a Formula Student monocoque. A stiffener is introduced to connect carbon fiber panels on both sides, and the geometry of the aluminum honeycomb connecting core is adjusted to improve the stress distribution in the joint panels. A finite element model under a three-point bending load is established based on the progressive damage model and the cohesive zone model. The mechanical properties were compared with conventional joints based on Formula Student three-point bending tests. Specimens were fabricated and tested using t700 carbon fiber prepreg and 3003 aluminum honeycombs to verify the joint’s performance and the accuracy of the finite element model. Experimental results showed that the three-point bending strength of the novel joint increased by 52.27%, and the stiffness increased by 101% compared to the conventional design. The simulated strength errors of the novel joint and the conventional joint were 4.66%, and 13.7%, respectively, and the failure modes were consistent with the experimental results, indicating the validity of the finite element model. The novel joint profile is less protruding than the conventional joint and could be widely used for joining or repairing automotive and aircraft components.
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Availability of Data and Materials
The data that support the findings of this study are available on request from the first author Yifei Wang. The data are not publicly available due to the studies are related to motorsports competitions, they contain information that may compromise the competitive advantage of the study participants in the competition.
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Appendix A
Appendix A
1.1 Mesh size sensitivity analysis
The SC8R shell element forms the skin of sandwich structures and joints. In order to study the influence of the mesh size on the simulation results in this model, the load–displacement curves of the three-point bending simulation were calculated when the mesh size changed from 0.5 mm to 2 mm, and the simulation time used was recorded, respectively. As can be seen from Fig. 20, when the cell size is 0.5 mm and 1 mm, the load–displacement curve is consistent with the experimental results, and the simulation results tend to converge. 1 mm mesh size can take into consideration both the requirements of calculation accuracy and calculation speed. With the increase of mesh size, the error of simulation results increases; when the mesh size is 2 mm, the results are not available.
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Wang, Y., Wang, F., Xu, Q. et al. Design and Analysis of a Novel Carbon Fiber Reinforced Polymer Sandwich Adhesive Joint. Appl Compos Mater 30, 791–813 (2023). https://doi.org/10.1007/s10443-023-10113-z
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DOI: https://doi.org/10.1007/s10443-023-10113-z