Modification of Eigenmodes in a Cold-Flow Rocket Combustion Chamber by Acoustic Resonators
Sign Up to like & getrecommendations! 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 ... read more here.
Keywords: modification eigenmodes; rocket combustion; combustion chamber; eigenmodes cold ... See more keywords