Vortex Shedding Induced Sound Inside a Cold-Flow Simulation of Segmented Chamber
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 2074
2. University of Utah, Salt Lake City, Utah 84112-9208
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.6110
Reference36 articles.
1. Stability of Longitudinal Oscillations with Pressure and Velocity Coupling in a Solid Propellant Rocket
2. Excitation of acoustic modes in a chamber by vortex shedding
3. Vortex Shedding as a Source of Acoustic Energy in Segmented Solid Rockets
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