Large Eddy Simulation of the fuel transport and mixing 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 fuel transport and mixing process in a scramjet combustor with rearwall-expansion cavity

Published:2016-09 Issue: Volume:126 Page:375-381
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Cai Zun,Liu Xiao,Gong Cheng,Sun Mingbo,Wang Zhenguo,Bai Xue-Song

Funder

National Natural Science Foundation of China

National University of Defense Technology

China Scholarship Council

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. Scramjet engines: the first forty years;Curran;J. Propuls. Power,2011

2. X-43A hypersonic veihicle technology development;Voland;Acta Astronaut.,2006

3. Detonation engine fed by acetylene–oxygen mixture;Smirnov;Acta Astronaut.,2014

4. Influencing factors on the mode transition in a dual-mode scramjet;Yan;Acta Astronaut.,2014

5. Classifier utility modeling and analysis of hypersonic inlet start/unstart considering training data costs;Chang;Acta Astronaut.,2011

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