Compressive response of honeycombs under in-plane uniaxial static and dynamic loading, Part 2: Simulations

被引：13

作者：

Chung, J ^{[1
]}

Waas, AM ^{[1
]}

机构：

[1] Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA

来源：

AIAA JOURNAL | 2002年 / 40卷 / 05期

关键词：

D O I：

10.2514/2.1736

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The static and dynamic experimental results of polycarbonate circular cell honeycombs subjected to in-plane uniaxial loading are simulated through numerical analysis using the finite element method. The experimental results were presented in Part 1 (Chung, J., and Waas, A. M., "Compressive Response of Honeycombs Under In-Plane Uniaxial Static and Dynamic Loading, Part 1: Experiments," AIAA Journal, Vol. 40, No. 5, 2002, pp. 966-973). Through a comparison between the experimental results and numerical analysis, the crushing mechanism of the circular cell honeycomb material is studied. The influence of friction between the loading plate and the honeycomb material is studied numerically in the simulation of the dynamic experimental results.

引用

页码：974 / 980

页数：7

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