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Effect of Cavity Width on the Unsteady Pressure in a Low-Mach-Number Cavity

โœ Scribed by Zhang, Ke; Naguib, Ahmed M.

Book ID
120994409
Publisher
American Institute of Aeronautics and Astronautics
Year
2008
Tongue
English
Weight
482 KB
Volume
46
Category
Article
ISSN
0001-1452

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Shallow cavities exposed to unbounded, low Mach number flow are generally weak aeroacoustic sources because their acoustic modes are heavily damped. This paper focuses on a cavity mounted on the wall of a duct to investigate the effect of ''confinement'', i.e., solid boundaries close to the cavity,