Investigation on Mechanical Properties and Equivalent Model of Aluminum Honeycomb Sandwich Panels
Investigation on Mechanical Properties and Equivalent Model of Aluminum Honeycomb Sandwich Panels
复制标题
铝蜂窝夹芯板力学性能及等效模型研究
DOI:
10.1007/s11665-018-3771-2
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发表时间:
2018-12-01
影响因子:
2.3
通讯作者:
Xu, Wei
中科院分区:
文献类型:
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作者:
Cai, Liangcai;Zhang, Duoyao;Xu, Wei
In this study, positive-pressure, bending, and drum peel tests were carried out for aluminum honeycomb sandwich panels made of different materials and with different dimensions. The results of these tests not only precisely revealed the relationships between the mechanical properties of aluminum honeycomb sandwich panels and the material dimensions of the face and core layers, the layout mode of the core layer, and the connecting mode between the face layers and core layers, but also determined the reliable mechanical equivalent model. The test results indicate that when the specimen was subjected to the vertical load, the compression properties of aluminum honeycomb sandwich panels were mainly determined by its core layer, while the face layer mainly relieves the axial stress and restrains the deformation of the core layer. In the flexural test, the face layer is the main part subjected to the load, whereas the core layer shows supporting, stabilizing, and strengthening effects, slowing the deformation of the face layer; flexural-tensile properties can be somewhat affected by the layout type of the core layer. The equivalent plate model, honeycomb plate model, and sandwich panel model were screened based on the experimental results, indicating that the sandwich panel model provided a more accurate description. The sandwich panel model was further modified, ultimately resulting in a more effective equivalent model that can accurately reflect the mechanical properties of the aluminum honeycomb sandwich panels.