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Published in 2019 at "Journal of Propulsion and Power"
DOI: 10.2514/1.b37405
Abstract: The influence of an absorber ring on the acoustics of a rocket combustion chamber is studied numerically and experimentally under nonreacting conditions. The transverse split modes that occur upon ...
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Keywords:
modification eigenmodes;
rocket combustion;
combustion chamber;
eigenmodes cold ... See more keywords