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蜂窝夹层结构具有优异的力学性能,被广泛的应用于航空航天领域,然而在其加工制备过程中易产生蜂窝芯子的脱焊等缺陷,蜂窝芯子缺陷对整个结构的力学性能产生不可忽略的影响,因此有必要对其产生的影响做出研究,本文研究了不同的蜂窝芯子脱焊尺寸在侧压载荷作用下对整体结构的影响。
The honeycomb sandwich structure has excellent mechanical properties and is widely used in the field of aerospace. However, defects such as desoldering of the honeycomb core tend to occur in the processing and preparation process, and the honeycomb core defects can not be neglected to the mechanical properties of the whole structure Therefore, it is necessary to make a study of the impact on the overall structure of the honeycomb core.