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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 ... Click to show full 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 ...
Keywords:
modification eigenmodes;
rocket combustion;
combustion chamber;
eigenmodes cold
Journal Title: Journal of Propulsion and Power
Year Published: 2019
Link to full text (if available)
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Journal Title: Journal of Propulsion and Power
Year Published: 2019
Link to full text (if available)
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recommendations!