摘要
阐述了固冲发动机燃气流量调节的必要性,对发生器燃气流量调节方案进行了评述.采用以改变喉面积来调节燃气流量的方案,对方案的静、动特性进行了分析.
The necessity of flow regulation system in solid ramjet is presented, and the scheme of gasfired flux adjustment about generator is analyzed. The gas-fired flux is adjusted, while throat area beening controlled. The static and dynamic characteristic of above scheme are analyzed.
出处
《战术导弹技术》
2009年第2期36-40,共5页
Tactical Missile Technology
基金
航空基金资助项目,编号:CB020802
