The Numerical Research on the Scramjet Combustion with Different Structure Cavity

Peng Gao; Xin Long Chang; Lei Luo; Yu Ji Cao

doi:10.4028/www.scientific.net/AMR.468-471.1444

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 468-471The Numerical Research on the Scramjet Combustion...

The Numerical Research on the Scramjet Combustion with Different Structure Cavity

Abstract:

In this paper, the detailed numerical simulations were performed in the hydrogen fuel combustion chamber with some different structure cavities. Through the analysis found that the effect of stabilized fire burning at supersonic flowing and mixed fuel and air are quite different. The research results will preferably represent the burning field in scramjet combustion so that the better performance flame stabilizer can be designed.

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Periodical:

Advanced Materials Research (Volumes 468-471)

Pages:

1444-1447

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.468-471.1444

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Online since:

February 2012

Authors:

Peng Gao, Xin Long Chang, Lei Luo, Yu Ji Cao

Keywords:

Cavity, Flame Stabilizer, Supersonic Combustion

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References

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