Numerical Analysis on Oscillation Characteristics in a Tailpipe Nozzle Solid Rocket Motor
Author:
Affiliation:
1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.48867
Reference28 articles.
1. Theory of Vortex Sound
2. Contributions to the theory of aerodynamic sound, with application to excess jet noise and the theory of the flute
3. Vortex generated sound in cavities
4. Effects of vorticity on rocket combustion stability
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