Acoustic energy exchange through flow turning
Author:
Affiliation:
1. U.S. Navy, Naval Research Laboratory, Washington, DC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-217
Reference61 articles.
1. Pulse-Triggered Instability in Solid Rocket Motors
2. Baum J.D. and Levine J.N. "Numerical Study of I flow turning Phenomenon," AIAA Preprint 86-0533, Presented at the AIAA 24`h Aerospace Sciences Meeting, Reno, Nv, Jan 6-9,1986.
3. Numerical simulation of the vortex-acoustic wave interaction in a dump combustor
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Study of the Flow Turning Loss in a Simulated Solid Rocket Motor;Journal of Propulsion and Power;1995-03
2. Effects of vorticity transport on combustion stability;22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference;1991-06-24
3. Investigation of flow turning phenomenon - Effects of frequency and blowing rate;27th Aerospace Sciences Meeting;1989-01-09
4. Acoustic-mean flow interaction in solid rocket motors using Navier-Stokes equations;24th Joint Propulsion Conference;1988-07-11
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