Large Eddy Simulation of the flame stabilization process in a scramjet combustor with rearwall-expansion cavity-Reference-Cited by-同舟云学术

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Large Eddy Simulation of the flame stabilization process in a scramjet combustor with rearwall-expansion cavity

Published:2016-11 Issue:42 Volume:41 Page:19278-19288
ISSN:0360-3199
Container-title:International Journal of Hydrogen Energy
language:en
Short-container-title:International Journal of Hydrogen Energy

Author:

Wang Zhenguo,Cai Zun,Sun Mingbo,Wang Hongbo,Zhang Yanxiang

Funder

National Natural Science Foundation of China

National University of Defense Technology

Publisher

Elsevier BV

Subject

Energy Engineering and Power Technology,Condensed Matter Physics,Fuel Technology,Renewable Energy, Sustainability and the Environment

Reference32 articles.

1. Scramjet propulsion (progress in Astronautics and Aeronautics);Curran,2000

2. Supersonic combustion experiments with a cavity-based fuel injector;Mathur;J Prop Power,2001

3. Cavity flame-holders for ignition and flame stabilization in scramjets: an overview;Ben-Yakar;J Prop Power,2001

4. Numerical simulation on ignition transients of hydrogen flame in a supersonic combustor with dual-cavity;Yang;Int J Hydrogen Energy,2016

5. Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor;Wang;Int J Hydrogen Energy,2013

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