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Numerical Simulation of Low Velocity Impact on Pin-Reinforced Foam Core Sandwich Panel

机译:低速冲击对销加强泡沫芯夹层板的数值模拟

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The use of sandwich structures is well established in industrial sectors where high stiffness and strength combined with lightweight are required, like in marine, wind turbine and railway applications. However, the vulnerability of sandwich structures to low-velocity impacts limits its use in primary aircraft structures. Pin reinforcement of the foam core enhances the out-of-plane properties and the damage tolerance of the foam core. In this paper, a finite element model is proposed to predict the impact behaviour of pin-reinforced sandwich structure. An approach based on the building block approach was used to develop the model. Multi-scale modelling in the impact region that considers the delamination of the face sheet using cohesive zone elements was employed to increase the accuracy of the simulation. Impact tests were performed to validate the numerical model. A good agreement between numerical and experimental results in terms of contact-force displacement history and failure mode was found.
机译:在工业领域中使用夹层结构的使用,需要高刚度和强度与轻质相结合,如海洋,风力涡轮机和铁路应用。然而,夹层结构对低速冲击的脆弱性限制了其在初级飞机结构中的应用。泡沫芯的引脚加固增强了平面外性质和泡沫芯的损伤容差。本文提出了有限元模型来预测销增强夹层结构的冲击性能。基于构建块方法的方法用于开发模型。采用多尺寸建模,以使用内聚区元件来考虑面板分层的撞击区域,以提高模拟的准确性。进行影响测试以验证数值模型。找到了在接触力位移历史和失败模式方面的数值和实验结果之间的良好一致性。

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