Qualitative model of vortex induced oscillations in a model of solid propellant boosters
Author:
Affiliation:
1. von Karman Inst. for Fluid Dynamics, Rhode-St.-Genese, Belgium
2. Eindhoven, Technische Univ., Netherlands
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2270
Reference12 articles.
1. Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces
2. Plateau, A. ; Van Moorhem, W. "Prediction of vortex shedding responses in segmented solid rocket motors",AIAAPaper 90-2073.
3. Cold flow investigation of the flow acoustic coupling in solid propellant boosters
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1. A combined time and frequency domain approach for acoustic resonance prediction;Journal of Sound and Vibration;2008-04
2. AERODYNAMICALLY GENERATED ACOUSTIC RESONANCE IN A PIPE WITH ANNULAR FLOW RESTRICTORS;Journal of Fluids and Structures;1999-08
3. Control of vortex-induced oscillations in a model solid rocket motor - Flow characterization and secondary injection experiments;35th Joint Propulsion Conference and Exhibit;1999-06-20
4. Cold flow simulation of vortex induced oscillations in a model of solid propellant boosters;5th AIAA/CEAS Aeroacoustics Conference and Exhibit;1999-05-10
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