Node-separation FEM simulation of typical spacecraft protective structure

被引：0
|
作者：
Zhang, Xiao-Tian [1 ]
Chen, Ying [2 ]
Jia, Guang-Hui [1 ]
Huang, Hai [1 ]
机构：
[1] School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
[2] Beijing Institute of Control Engineering, Beijing 100190, China
来源：
Yuhang Xuebao/Journal of Astronautics | 2013年 / 34卷 / 05期
关键词：
Finite element method;
D O I：
10.3873/j.issn.1000-1328.2013.05.001
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：597 / 604
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