Control Effects of Baffle on Combustion Instability in a LOX/GH2 Rocket Engine
Author:
Affiliation:
1. Academy of Equipment Command & Technology, 101416 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.46240
Reference28 articles.
1. Linear and non-linear pressure oscillations in baffled combustion chambers
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