The Influence of Supersonic Combustion when the Cavity Parameters Changed on the Chamber Wall

Peng Gao; Xin Long Chang; Shuang Lin Gao; Jie Tang Zhu

doi:10.4028/www.scientific.net/AMR.468-471.2620

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 468-471The Influence of Supersonic Combustion when the...

The Influence of Supersonic Combustion when the Cavity Parameters Changed on the Chamber Wall

Abstract:

In this paper, the detail numerical simulations were performed on the flow field of the scramjet combustor chamber with the hydrogen fuel, when the cavity parameters changed. The research results indicate that the effect of gas and air mixing and flame stability are altered when the parameter of cavity changed. From the research we will better understand the supersonic combustion. The high efficiency flame stabilities can be designed in future.

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Periodical:

Advanced Materials Research (Volumes 468-471)

Pages:

2620-2623

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.468-471.2620

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Online since:

February 2012

Authors:

Peng Gao, Xin Long Chang, Shuang Lin Gao, Jie Tang Zhu

Keywords:

Cavity Structure, Flame Stability, Supersonic Combustor

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References

[1] T.M. Abdel-Salam S.N. Tiwari: Study of Supersonic Combustion Characteristics in a Scramjet Combustor,AIAA2003-3550

Google Scholar

[2] Kumauro,T.Kudo: Experiment on a Rectangular Cross Section Scramjet Combustor, National Aerospace Lab NALTR-1068,Japan

Google Scholar

[3] E. T. Curran, S. N. B. Murthy: Scramjet Propulsion, Progress in Astronautics and Aeronautics, AIAA2001

Google Scholar

[4] Xiao.yinli,Song.wenyan,Chen.liang: Numerically Investigating Performance Gain in a Scramjet Combustor through Using Cavity, Journal of Northwestern Polytechnical University,(2009)

Google Scholar

[5] A de la Benyakar, Ronald K Hanson R K: Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets, An Overview. Journal of Propulsion and Power, 2001, 17 (4) : 869～ 577

DOI: 10.2514/2.5818

Google Scholar

[6] Faure J. Malo-Molina，Datta V. Gaitonde: Numerical Investigation of a 3-D Chemically Reacting Scramjet Engine at High Altitudes Using JP8 - Air Mixtures, AIAA2005-1435

DOI: 10.2514/6.2005-1435

Google Scholar

[7] Yang Shi-min, Tang Hao, Huang Yue: Numerical Simulation of Combustion Flow Field of Supersonic Combustor with Cavity, Journal of Aeroengine, Sep. 2008.

Google Scholar