Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine-Reference-Cited by-同舟云学术

Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine

Published:2014-10-13 Issue:6 Volume:18 Page:652-691
ISSN:1364-7830
Container-title:Combustion Theory and Modelling
language:en
Short-container-title:Combustion Theory and Modelling

Author:

Gao Zhenxun,Wang Jingying,Jiang Chongwen,Lee Chunhian

Publisher

Informa UK Limited

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,Modelling and Simulation,General Chemical Engineering,General Chemistry

Link

http://www.tandfonline.com/doi/pdf/10.1080/13647830.2014.962617

Reference44 articles.

1. R.A. Baurle,Modelling of high speed reacting flows: Established practices and future challenges, 42nd AIAA Aerospace Sciences Meeting and Exhibit, 5–8 January 2004, Reno, NV, AIAA Paper No. 2004–267.

2. Turbulent combustion modeling

3. Flame structures and combustion efficiency computed for a Mach 6 scramjet engine

4. Investigation of the effect of chemistry models on the numerical predictions of the supersonic combustion of hydrogen

5. Assumed PDF turbulence-chemistry closure with temperature-composition correlations

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