Experimental investigations on H2/air rotating detonation wave in the hollow chamber with Laval nozzle-Reference-Cited by-同舟云学术

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Experimental investigations on H2/air rotating detonation wave in the hollow chamber with Laval nozzle

Published:2017-02 Issue:5 Volume:42 Page:3363-3370
ISSN:0360-3199
Container-title:International Journal of Hydrogen Energy
language:en
Short-container-title:International Journal of Hydrogen Energy

Author:

Zhang Hailong,Liu Weidong,Liu Shijie

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

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

Reference37 articles.

1. Liquid rocket engine combustion instability;Yang;Prog Astronaut Aeronaut Ser AIAA J,1995

2. Liquid rocket thrust chambers: aspects of modeling, analysis, and design;Yang;Prog Astronaut Aeronaut AIAA J,2004

3. Combustion instabilities in liquid rocket engines: testing and development practices in Russia;Dranovsky;Prog Astronaut Aeronaut Ser AIAA J,2007

4. Control effects of baffle on combustion instability in a LOX/GH2 rocket engine;Feng;J Spacecr Rockets,2010

5. Experimental study on propagation mode of H2/Air continuously rotating detonation wave;Lin;Int J Hydrogen Energy,2015

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