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Transmission of sound across a vortex layer enclosing a cylindrical column of jetAn approximate solution to the problem of transmission of sound across a cylindrical vortex was obtained. Results are considerably different from the plane vortex sheet case because of the added role played by the curvature of the jet. In comparison with the plane case, the specularly transmitted waves are more complex and require some numerical integration. Resonance waves are identically predicted for M 2, but there is also a wave field whose modified effect appears to extend the region of resonance just as the instability waves cover a region in space and time. The instability waves are predicted to exist for all Mach numbers but vanish for wavelengths that are large compared to the jet radius. The region of propagation is similarly wavelength dependent.
Document ID
19830010136
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Luh, R.
(Stanford Univ. CA, United States)
Chao, C. C.
(Stanford Univ. CA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1982
Subject Category
Acoustics
Report/Patent Number
NAS 1.26:169845
SU-JIAA-TR-50
NASA-CR-169845
Report Number: NAS 1.26:169845
Report Number: SU-JIAA-TR-50
Report Number: NASA-CR-169845
Accession Number
83N18407
Funding Number(s)
CONTRACT_GRANT: NCC2-76
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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