摘要
本文应用振荡燃烧的线性理论,从理论上预计到不能用H-burner测量低频速度耦合响应函数,并且通过实验验证了此论断的正确性.
In this paper it is predicted with the linearizing theory of oscillatory combustion that H-burner can not be used to measure the coupling response function of low-frequency oscillation. The conclution is also proved by many experiments
出处
《推进技术》
EI
CAS
CSCD
北大核心
1990年第2期23-28,共6页
Journal of Propulsion Technology
关键词
固体推进剂
火箭发动机
振荡燃烧
Solid rocket engine, Low frequency, Oscillation burning
