Experimental Study of Shear-Layer/Acoustics Coupling in Mach 5 Cavity Flow
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1319
Reference25 articles.
1. An Investigation of Separated Flows - Part I: The Pressure Field
2. Review—Self-Sustaining Oscillations of Flow Past Cavities
3. Perng, S. W. “Passive Control of Pressure Oscillations in Hypersonic Cavity Flow,” Ph.D. Dissertation, Dept. of Aerospace Engineering and Engineering Mechanics,Univ. of Texas, Austin, TX,Dec. 1996.
4. The physical mechanism of flow-induced pressure fluctuations in cavities and concepts for their suppression
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