Flow Field Characteristics of Butterfly-Type Cavity and its Influence on Supersonic Flow

Jin Xiang Wu; Jing Ma; Xiang Gou; Lian Sheng Liu; En Yu Wang

doi:10.4028/www.scientific.net/AMR.347-353.2468

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Catalytic Fast Pyrolysis of Cellulose with HZSM-5
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Flow Field Characteristics of Butterfly-Type Cavity and its Influence on Supersonic Flow
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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 347-353Flow Field Characteristics of Butterfly-Type...

Flow Field Characteristics of Butterfly-Type Cavity and its Influence on Supersonic Flow

Abstract:

A new type of cavity configuration — butterfly-type cavity applied in the scramjet is proposed in this paper. The supersonic combustion chamber with Butterfly-type cavity was investigated numerically and experimentally. Results show that the horizontal vortex moving along the Y direction is helpful in gathering hydrogen gas, but the vertical vortex moving along the Z direction is not. Both turbulent kinetic energy and turbulent kinetic energy dissipation rate are very high at the junction between the cavity and the main combustion chamber. And the production of turbulent kinetic energy is agreeable with that of turbulent kinetic energy dissipation.

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Periodical:

Advanced Materials Research (Volumes 347-353)

Pages:

2468-2474

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.347-353.2468

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Online since:

October 2011

Authors:

Jin Xiang Wu, Jing Ma, Xiang Gou, Lian Sheng Liu, En Yu Wang

Keywords:

Butterfly-Type Cavity, Flow Field, Supersonic Flow, Vortex

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References

[1] Juan Liu, Yu Pan, Weidong Liu and Zhenguo Wang:Journal of Aerospace Power. Vol.24 (2009) , P.2501 (In Chinese)

Google Scholar

[2] Juan Liu, Yu Pan, Weidong Liu and Zhenguo Wang:Journal of National University of Defense Technology. Vol.31(2009),P.5 (In Chinese)

Google Scholar

[3] Yu Pan, Meng Ding, Jianhan Liang andZhenguo Wang:Acta Aeronautica Et Astronautica Sinica. Vol.31(2010),P.70 (In Chinese)

Google Scholar

[4] Rasmussen. C. C. Driscoll. J. F. and Carter. C. D. et al:Journal of Propulsion and Power. Vol.21 (2004),P 765

Google Scholar

[5] R. A. Baurle. D. R. Eklund:Journal of Propulsion and Power.Vol.18 (2002),P 990

Google Scholar

[6] Rasmussen. C. C. Driscoll. J. F. and Carter. C. D. et al:Journal of Propulsion and Power. Vol.21 (2004),P765

Google Scholar

[7] Jeong-Yeol Choi. Fuhua Ma. Vigor Yang:Proceedings of the Combustion Institute.Vol.30 (2005), P2851

Google Scholar

[8] M.R. Gruber R.A. Baurle.T.Matbur.K.-Y Hsu: Journal of Propulsion and Power. Vol.17 (2001), P146

Google Scholar

[9] Daniel J. Mickie,James F:Proceedings of the Combustion Institute. Vol.32 (2009),P. 2397

Google Scholar

[10] K. H. Yu,K. C. Schadow:Combustion and Flame, Vol. 99(1994), P. 295

Google Scholar

[11] Ben-Yakar Adela, Natan Benveniste and Gany Alon:Propul.Power. Vol.14 (1998),P 447

Google Scholar