Influence of radial injected flow on the aeroacoustic coupling in solid propellant boosters
Author:
Affiliation:
1. von Karman Inst. for Fluid Dynamics, Rhode-St.-Genese, Belgium
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2101
Reference14 articles.
1. Vortex Shedding as a Source of Acoustic Energy in Segmented Solid Rockets
2. Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces
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3. Comparison of Different Passive Control Solutions for Reducing SRM Pressure Oscillations Using Cold Flow Experiments;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21
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