[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 >

2012 , Vol. 32 >Issue 6: 99 - 102

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.06.018

ROCKETS TECHNOLOGY

Numerical Simulation of Bluff-body Structural Parameters in Advanced Vortex Combustor

  • SUN Haijun ,
  • ZENG Zhuoxiong ,
  • XU Yihua
Expand
  • Aircraft Engineering College, Nanchang Hangkong University, Nanchang 330063, China

Received date: 2012-02-23

  Online published: 2025-05-29

Fold

Abstract

In order to study the best matching relation of bluff-body structural parameters in advanced vortex combustor (AVC), numerical simulation on the cold state flow in combustor was carried out. The results indicate that the combustor has better flow characteristics by the layout of bluff-body presented in model I, when the equivalent ratios of structural parameters are H₁/H2 =0.7 and S/H₁ = 0.6, total pressure loss coefficient is lower and stability of vortex is stronger. The selection rule of structural parameters in AVC can not copy totally from the stability of vortex formation structure relation in Trapped Vortex Combustor (TVC) .

Key words： ramjet; vortex combustor; structural parameters; turbulence; total pressure loss

Cite this article

SUN Haijun , ZENG Zhuoxiong , XU Yihua . Numerical Simulation of Bluff-body Structural Parameters in Advanced Vortex Combustor[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(6) : 99 -102 . DOI: 10.15892/j.cnki.djzdxb.2012.06.018

[an error occurred while processing this directive]

References

[1]
Hsu KY, Goss LP, Trump D D, et al. Performance of atrapped-vortex combustor[C] //AIAA 33rd Aerospace Sciences Meeting and Exhibit, 1995.
[2]
KENDRICK DW, CHENEVERT B C, TRUEBLOOD B, et al. Combustion system development for the ramgen engine[J]. Journal of Engineering for Gas Turbines and Power,2003(7):885-894.
[3]
Edmonds R G, Steele RC, Williams JT, et al. Ultra-lowNOx advanced vortex combustor[C] // Proceedings of theASME Turbo Expo 2006, Power for Land, Sea and Air,2006:255-262.
[4]
邓洋波, 刘世青, 钟兢军. AVC中钝体布置与燃烧室流动特性研究[J].工程热物理学报,2008,29(8):1416- 1418.
[5]
邓洋波, 刘世青, 钟兢军. 先进旋涡燃烧室燃烧特性数值模拟[J].大连海事大学学报,2008,34(3):21-24.
[6]
Roquemore W, Shouse D, Burrus D, et al. Trapped vortexcombustor concept for gas turbine engines[C] // 39thAIAA Aerospace Sciences Meeting and Exhibit, Reno, Ne-vada, 2001, 0483.
[7]
邓洋波, 刘世青, 钟兢军. 先进旋涡燃烧室流动与燃烧特性分析[J].航空动力学报,2009, 24(3): 488-493.
[8]
钟兢军, 刘世青. 后驻体喷孔位置对驻涡腔流动冷态数值的影响.上海海事大学学报,2011, 32(1):44-48.
Options
Outlines

/

〈 〉

[an error occurred while processing this directive]