推进技术 ›› 1990, Vol. 11 ›› Issue (2): 23-28.
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王宁飞,孙维申,胡竞岩
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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.
关键词: 固体火箭发动机;低频;振荡燃烧
Abstract: 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
Key words: Solid rocket engine;Low frequency;Oscillation burning
王宁飞,孙维申,胡竞岩. 亥姆霍兹燃烧器测量低频速度耦合响应函数可行性问题的探讨[J]. 推进技术, 1990, 11(2): 23-28.
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