摘要
利用局部动力相似理论，对贮运箱式导弹发射箱在后密封盖封闭状态下，静态点火时内部流场的变化情况进行了实验研究，发现在弹管间隙内存在着新的流场结构，以及这种流场结构随后密封盖开启时间而变化的规律。
The internal exhaust flow field of closed rectangular missile launch tube is studied by using local dynamic similiarity theory. A new construction of flow field is found in the space between the tube-wall and missile. A rule of the new construction changing with the open-time is also put forward in this thesis.
出处
《弹道学报》
CSCD
1995年第2期52-56,共5页
Journal of Ballistics
关键词
发射箱
内流场
燃气流特性
导弹
closed launch tube, internal flow, experimental study
