Combustion Stability Boundaries of the Subscale Rocket Chamber with Impinging Jet Injectors
Author:
Affiliation:
1. Chosun University, Gwangju 501-759, Republic of Korea
2. Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea
3. Research Institute of Chemical Machine Building (NIICHIMMASH), 141300, Sergiev Posad, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.19937
Reference24 articles.
1. A review of active control of combustion instabilities
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