航空兵器Issue(1)：37-39,47,4.
固体推进剂结构完整性分析数值仿真的研究发展
Current Situati on and Trend of Structure Integrity Analysis of Solid Propellant
李冲冲 1郭颜红 1肖志平2
作者信息
- 1. 中国空空导弹研究院，河南洛阳 471009
- 2. 航空制导武器航空科技重点实验室，河南洛阳 471009
- 折叠
摘要
Abstract
The analysis of the structure integrity of solid propellants is summarized .The methods for structure integrity analysis are reviewed, the applications of numerical simulation in the analysis of solid propellant structure integrity are introduced especially .The difficulties of numerical simulation analysis caused by the propellant mechanical properties and the complexity of load environment are explained .The achievements and the development trend in the future of using numerical simulation analysis in the study of solid propellant structure integrity are presented .关键词
固体推进剂/结构完整性/数值仿真Key words
solid propellant/structure integrity/numerical simulation分类
航空航天引用本文复制引用
李冲冲,郭颜红,肖志平..固体推进剂结构完整性分析数值仿真的研究发展[J].航空兵器,2014,(1):37-39,47,4.
