摘要
针对一种用于液体火箭发动机的稳流型流量调节器，在理论建模的基础上，对其动态响应特性进行了计算机仿真，得到了该型流量调节器的阶跃响应和幅频响应特性，并研究了调节器阻尼系数的选择对其阶跃响应和幅频响应特性的影响。
A new type of output flow stabilized regulator used in high pressure staged combustion liquid propellant rocket engines is introduced.And on the basis of theoretical modeling,the characteristics of the step response and amplitude frequency response of the flow regulator were investigated by means of computer simulation.The effect of damping coefficient was also investigated
出处
《推进技术》
EI
CAS
CSCD
北大核心
1999年第1期60-64,共5页
Journal of Propulsion Technology
关键词
液体推进剂
火箭发动机
流量调节器
动态响应
Liquid propellant rocket engine,Flow regulator,Dynamic response,Computerized simulation
