| Citation: |
DENG Xiaoxing, ZHU Zixu, CHEN Changhai, et al. Research status of quasi-static stability performance of composite sandwich structures[J]. Acta Materiae Compositae Sinica, 2024, 41(11): 5701-5723. DOI: 10.13801/j.cnki.fhclxb.20240325.003
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Composite sandwich structures are widely used in aerospace, shipbuilding and other fields due to their excellent strength- and stiffness-to-weight ratio and small apparent density. From the three aspects of theoretical research, simulation analysis and experimental research, this paper summarizes the current situation of quasi-static stability research of honeycomb, foam, lattice and foldcore sandwich structures. The research on honeycomb sandwich structure is relatively mature, and further research should focus on the application field. The foam sandwich structure needs to be strengthened in the panel/core interface, and the fiber stitching technology can be considered. The theory of foldcore sandwich structure needs further study and has great potential. The lattice sandwich structure has stronger anti-buckling ability than other structures, but there is still a problem of face/core bonding. The problem of the quasi-static stability of the composite sandwich structure is mainly focused on the bonding of the face/core. The fiber stitching technology can effectively enhance the performance of the face/core. The research in this area has a strong potential for enhancing the stability of the composite sandwich structure.
Composite sandwich structures are a type of construction that utilizes composite materials as face sheets and lightweight materials as the core layer, forming a sandwich structure. Due to their advantages of being lightweight and high-strength, they are widely applied in various fields such as aerospace, aviation, and shipbuilding. With the application of composite sandwich structures in pressure-resistant structures, the study of their stability has become increasingly important. Researching the quasi-static stability of composite sandwich structures is of significant importance for the design technology of these structures and for expanding the application range of the materials. Therefore, this article reviews and summarizes the current research status on the quasi-static overall stability and panel stability under in-plane loads and axial compressive loads for four typical sandwich structures: honeycomb core structures, foam core structures, lattice core structures, and corrugated core structures. It also analyzes the characteristics and advantages of each typical structure, aiming to provide a reference for future related research.
The article begins by illustrating the four typical sandwich structures and briefly discussing their current application status. The core review is divided into three parts: theoretical research, simulation analysis, and experimental research. Theoretical research starts from general to specific, initially providing an overview and analysis of three general laminated plate theory models. It then proceeds to review and summarize the theoretical models of the four special sandwich structures. Simulation analysis directly starts with the four special sandwich structures, discussing the simulation models for each, the details of the methods used, the strengths and weaknesses of the models, and concludes with a summary and generalization at the end of the section. Experimental research, similar to simulation analysis, discusses the experimental studies related to the four typical sandwich structures. The article focuses on reviewing the objectives and methods of the experiments, the characteristics of the structures, and so on.
From the perspectives of theoretical research, simulation analysis, and experimental research, the following observations can be made:1. The maturity of laminated plate theory research makes the use of homogenization and equivalent methods a mainstream direction in theoretical research. The progress of theoretical research on various cores varies, especially in the areas of stitching techniques for foam core structures and theoretical research on corrugated core structures, which require further exploration.2. Due to the complex failure mechanisms of composite materials, it is challenging to establish accurate numerical prediction models for numerical simulation, and internal defects are difficult to simulate. However, under the premise of validating methods, repeated simulation experiments can be conducted at a low cost. Therefore, using numerical simulation to replace some experiments can effectively improve efficiency and save costs.3. In terms of experimental results, honeycomb cores exhibit strong resistance to out-of-plane compressive loads, with failure modes characterized by local buckling of the core walls. When subjected to in-plane compressive loads, they are prone to overall buckling instability. Foam cores have a significant advantage in bending resistance at equal density. Lattice core structures have a clear boundary between instability and collapse under compression loads, which is conducive to advancing research on stability. Corrugated core structures show a clear advantage in resisting local buckling and have a high degree of design flexibility, offering greater potential in terms of bending stiffness.Conclusions: This article provides a comprehensive review of the theoretical research, simulation analysis, and experimental studies on the static stability of four typical sandwich structures. Given the outstanding designability of composite sandwich structures, their future prospects in stability design applications are promising, especially in the design and application of corrugated core structures, which warrant further research and exploration. The development of fiber stitching technology has offered a feasible solution to the weak interface issues between the face and core of composite sandwich structures. In addition, the diversification of structures, the broadness of application prospects, the innovation in manufacturing processes, and the automation in production will all be hot topics for future research.
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