Effect of Nozzle Cavity on Resonance in Large SRM: Numerical Simulations
Author:
Affiliation:
1. von Karman Institute for Fluid Dynamics, 1640 Rhode-St-Genese, Belgium
2. SNPE, 91710 Vert-le-Petit, France
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/10.2514/2.6141
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1. Vortex Shedding as a Source of Acoustic Energy in Segmented Solid Rockets
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