摘要
采用局部动力相似理论建立了火箭炮同时离轨发射系统的静态模拟实验，对发射管内二次流进行了实验研究，摸清了管内二次流的流动特征。
A static simulation experiment for a non-tip-off rocket launch tube has been carried out,making use of the theory of local dynamic similiarity.Some experimental work on the secondary flow within the launch tube has been done,and characteristics of the secondary flow in the annular gap between the rocket body and the launch tube have been clearly elucidated.
出处
《兵工学报》
EI
CAS
CSCD
北大核心
1994年第2期75-77,共3页
Acta Armamentarii
关键词
火箭
发射管
二次流
实验研究
rocket,launch tube,secondary flow,experimental study
