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Journal of Projectiles, Rockets, Missiles and Guidance >

2011 , Vol. 31 >Issue 2: 120 - 122

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.02.032

ROCKETS TECHNOLOGY

Numerical Analysis of Plume Field for SRM with Gas Vane

  • MO Zhan ,
  • BAI Taotao ,
  • GUO Yanhong
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2010-05-29

  Online published: 2025-05-30

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Abstract

The plume field of solid rocket motor (SRM) with gas vane is much more complex than the one without the gas vane. The plume fields at the different altitude with the same free stream Mach number were compared by numerical simulation. The axis section of the SRM's plume field with gas vane is cross-shaped. The plume field and temperature boundary expands with the altitude increase. The length of the plume field is about 200 fold of nozzle's outlet diameter.

Key words： SRM; gas vane; plume field; numerical simulation

Cite this article

MO Zhan , BAI Taotao , GUO Yanhong . Numerical Analysis of Plume Field for SRM with Gas Vane[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(2) : 120 -122 . DOI: 10.15892/j.cnki.djzdxb.2011.02.032

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References

[1]
李军, 曹从咏, 徐强. 固体火箭发动机羽流场特性的数值研究[J]. 弹箭与制导学报, 2003, 23(2): 307-312.
[2]
张福祥. 火箭燃气射流动力学[M]. 北京: 国防工业出版社, 1988.
[3]
赵承庆. 气体射流动力学[M]. 北京: 北京理工大学出版社, 1998.
[4]
李军, 李献伟. 推力矢量发动机射流流场的数值分析[J]. 弹箭与制导学报, 2005, 25(4): 80-82.
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