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The Turbulent Boundary-Layer Rough-Wall Pressure Spectrum at Acoustic and Subconvective Wavenumbers

✍ Scribed by Howe, M. S.

Book ID
120149071
Publisher
The Royal Society
Year
1988
Tongue
English
Weight
494 KB
Volume
415
Category
Article
ISSN
0962-8444

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Aircraft cabin noise due to the fuselage boundary layer is determined by, among other factors, the wavenumber-frequency spectrum of the fluctuating boundary layer pressures, a quantity for which a number of models have been proposed. In this work predictions for the sound radiated by a boundary laye