摘要
对垂直发射装置燃气流的低频不稳定性进行了分析,给出了压力振荡与温度振荡二者之间数学表达式,并给出了定性的实验证明本文首次测得了燃气流温度整体振荡。
An analysis is presented in which the instability known as low-frequency of hot gas flow is studied in the vertical launching system.A mathematical model is obtained about the relationship between pressure oscillation and temperature oscillation and a quantitative experimental result is given.These experimental data about the temperature perturbation of low-frequency whole oscillations are first obtained in the experiment .It shows that it is not light considering whole oscillation as equal temperature.
出处
《哈尔滨工程大学学报》
EI
CAS
CSCD
1997年第2期27-32,共6页
Journal of Harbin Engineering University
关键词
发射装置
压力振荡
温度振荡
导弹
垂直发射装置
launching system
low-frequency instability
pressure oscillation
temperature oscillation