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Acoustic resonances and sound scattering by a shear layerThe energy reflection coefficient is evaluated numerically for plane waves incident on a plane shear layer having a linear velocity profile. The shear layer is found to exhibit no resonances and no Brewster angles. The behavior of the reflection coefficient depends crucially on the parameter tau, a nondimensional measure of the disturbance Strouhal number with respect to the disturbance Mach number in the mean flow direction. For moderate values of tau, the amplified reflection regime degenerates into the total reflection one, whereas in the ordinary reflection regime the variation of the reflection coefficient with tau depends on whether or not the corresponding vortex sheet has a Brewster angle. The results indicate that caution should be exercised in uncritically modeling a finite thickness shear layer by a corresponding vortex sheet.
Document ID
19800007613
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Koutsoyannis, S. P.
(Stanford Univ. CA, United States)
Karamcheti, K.
(Stanford Univ. CA, United States)
Galant, D. C.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1979
Subject Category
Acoustics
Report/Patent Number
NASA-CR-166181
SU-JIAA-TR-20
Report Number: NASA-CR-166181
Report Number: SU-JIAA-TR-20
Accession Number
80N15873
Funding Number(s)
CONTRACT_GRANT: NSG-2233
CONTRACT_GRANT: NSG-2308
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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