[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

Journal of Projectiles, Rockets, Missiles and Guidance >

2011 , Vol. 31 >Issue 2: 123 - 126

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.02.033

ROCKETS TECHNOLOGY

The Adjusting Valve Design and Adjusting Performance Study for Solid-rocket Ramjet Motor

  • HOU Xiaojing ,
  • MO Zhan
Expand
  • Chian Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2010-07-01

  Online published: 2025-05-30

Fold

Abstract

Two kinds of flux control valves including the arc one and the taper one were designed by designing calculation. The flow performances of the two kinds of control valves were very similar in the same working state after the 3-D numerical simulation, and the arc valve was better for flow control after the analysis of the characteristics of the two kinds of valves whose pressure was related with the valves' displacement. The investigation would be helpful for flux adjustment for solid rocket ramjet motor.

Key words： flux control; flux control valve; adjustment performance; numerical simulation

Cite this article

HOU Xiaojing , MO Zhan . The Adjusting Valve Design and Adjusting Performance Study for Solid-rocket Ramjet Motor[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(2) : 123 -126 . DOI: 10.15892/j.cnki.djzdxb.2011.02.033

[an error occurred while processing this directive]

References

[1]
鲍福廷, 黄熙君, 张振鹏,等. 固体火箭组合发动机[M]. 北京: 中国宇航出版社, 2006.
[2]
鲍文, 牛文玉, 陈林泉,等. 固体火箭冲压发动机燃气流量调节特性[J]. 推进技术, 2007, 28(4): 99-102.
[3]
李岩芳, 陈林泉. 固冲燃气发生器流量调节数值模拟研究[C]// 西安: 中国宇航学会固体火箭推进专业委员会2001年年会, 2001.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]