航天器环境工程2018，Vol.35Issue(3)：210-216,7.DOI:10.3969/j.issn.1673-1379.2018.03.002
超高速撞击中靶后碎片云的内外边界方程研究
The inner and outer boundary equations of hypervelocity impacted debris cloud behind the shield
贾光辉 1刘巧霞 1张榜1
作者信息
- 1. 北京航空航天大学 宇航学院,北京 100191
- 折叠
摘要
Abstract
A better understanding of the behavior of the debris cloud model under the hypervelocity impact is important for designing the shield structure of spacecraft. In this paper, a numerical simulation method is proposed to study the inner and outer boundary model of the debris cloud. According to its origin, the debris cloud is classified into the target cloud and the projectile cloud. The inner and outer boundaries of the cloud shape are determined according to the distribution characteristics of each cloud. The curves of Bernoulli's lemniscates are modified into a combination of lemniscates and circles. It is shown that the modified curves are more appropriate to fit the actual debris shape than the lemniscates.关键词
超高速撞击/碎片云/数值仿真/双纽线/内外边界方程Key words
hypervelocity impact/debris cloud/numerical simulation/lemniscates/inner and outer boundary equations分类
航空航天引用本文复制引用
贾光辉,刘巧霞,张榜..超高速撞击中靶后碎片云的内外边界方程研究[J].航天器环境工程,2018,35(3):210-216,7.
