Yin Yufan, Zhang Xiaojing
School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China.
Materials (Basel). 2024 Aug 13;17(16):4024. doi: 10.3390/ma17164024.
To optimize the assembly methods of honeycomb structures and enhance their design flexibility, this study investigated the impact mechanical responses of tandem honeycomb-core sandwich structures with varying misalignment assembly lengths. Impact tests were conducted across different energy levels on single-layer and tandem honeycomb-core sandwiches to observe their impact processes and failure behaviors. Our findings indicate that tandem honeycomb cores significantly enhance the impact resistance compared with single-layer configurations, even though a misaligned assembly can deteriorate this property. A finite element model was developed and validated experimentally; the model showed good agreement with the experiments, thereby allowing the simulation and evaluation of the impact responses. Herein, we reveal that specific misalignment lengths can either increase or decrease the impact resistance, providing insights into improving the resilience of tandem honeycomb-core structures. Our results not only contribute to enhancing the impact resistance of honeycomb-core sandwich structures but also offer a valuable basis for their practical applications in engineering.
为了优化蜂窝结构的组装方法并提高其设计灵活性,本研究调查了不同错位组装长度的串联蜂窝芯夹层结构的冲击力学响应。在不同能量水平下对单层和串联蜂窝芯夹层进行了冲击试验,以观察其冲击过程和失效行为。我们的研究结果表明,与单层结构相比,串联蜂窝芯显著提高了抗冲击性,尽管错位组装会降低这一性能。开发了一个有限元模型并通过实验进行了验证;该模型与实验结果吻合良好,从而能够对冲击响应进行模拟和评估。在此,我们揭示了特定的错位长度可以增加或降低抗冲击性,为提高串联蜂窝芯结构的韧性提供了见解。我们的结果不仅有助于提高蜂窝芯夹层结构的抗冲击性,也为其在工程中的实际应用提供了有价值的依据。