In this paper, by modeling a actual foam sandwich panel, the aluminum foam sandwich simplifiedas standard honeycomb is preliminarily proved feasible.
最后再针对其他试验工况，将修正后的有限元模型与实验结果比对，以验证标准蜂窝结构来模拟泡沫铝夹芯的可行性。
The quasi-static and dynamic compression mechanical properties of sandwich panel with aluminum foam core have been studied in this paper.
本文对泡沫铝芯体夹层板材的准静态和动态力学性能进行了试验研究。
The quasi-static and dynamic compression mechanical properties of sandwich panel with aluminum foam core have been studied in this paper.
本文对泡沫铝芯体夹层板材的准静态和动态力学性能进行了试验研究。
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