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Failure study of honeycomb sandwich structure with embedded part under axial pullout loading

机译:轴向拉力作用下带嵌件蜂窝夹芯结构的破坏研究

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The deformation and failure behavior of a regular hexagonal honeycomb sandwich structure with an embedded part under axial pullout loading are studied. The deformation process of the honeycomb sandwich structure was recorded using a noncontact full-field optical measurement method based on three-dimensional digital image correlation. A corresponding finite element numerical model of the honeycomb sandwich structure with embedded parts is established. A cohesive zone model is used to simulate the interface failure of the honeycomb sandwich structure with the embedded part. The four groups of interface parameters were characterized by standard testing procedures including the flatwise tensile test, single-lap test, double cantilever beam test and three-point bending test. The numerical results accurately predicted the ultimate load of the structure. The failure process and failure mechanism of the honeycomb sandwich structure with the embedded part are obtained. The combination of an experiment and numerical methods effectively revealed the deformation and failure behavior of honeycomb sandwich structures with an embedded part under axial pullout loading.
机译:研究了规则的六边形蜂窝夹层结构在轴向拉拔载荷作用下的变形和破坏行为。使用基于三维数字图像相关性的非接触式全场光学测量方法记录了蜂窝状夹层结构的变形过程。建立了具有嵌入式零件的蜂窝夹层结构的相应有限元数值模型。内聚区模型用于模拟蜂窝夹层结构与嵌入式零件的界面破坏。通过标准测试程序对四组界面参数进行了表征,其中包括水平拉伸测试,单搭接测试,双悬臂梁测试和三点弯曲测试。数值结果准确地预测了结构的极限载荷。获得了具有嵌入式部件的蜂窝夹层结构的破坏过程和破坏机理。实验和数值方法的结合有效地揭示了在轴向拉拔载荷作用下带有嵌入式零件的蜂窝夹层结构的变形和破坏行为。

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