A Vortex Shedding-Based Combustion Response Model Applied to an Unstable Liquid Rocket Combustor
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ; 2009 ; Denver , Colorado
2009-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Acoustics, Vortex Shedding, and Low-Frequency Dynamics Interaction in an Unstable Hybrid Rocket
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