Transient flow characteristics and performance of a solid rocket motor with a pintle valve

被引:0
|
作者
SONG, Anchen [1 ]
WANG, Ningfei [1 ]
LI, Junwei [1 ]
MA, Baoyin [1 ]
CHEN, Xinjian [1 ]
机构
[1] School of Aerospace, Beijing Institute of Technology, Beijing,100081, China
来源
Chinese Journal of Aeronautics | 2020年 / 33卷 / 12期
关键词
36;
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中图分类号
学科分类号
摘要
Journal article (JA)
引用
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页码:3189 / 3205
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