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Effects of noise radiated from convected ring sources in coaxial dual flow. Part 1: The noise from unheated jetsThe effects of flight on sound radiated from embedded, uncorrelated ring sources convecting along the midst of the primary and the secondary streams of a coaxial dual flow which emerges from a moving nozzle into the ambience are studied. Cold jets are examined. The problem is posed as a double vortex-sheet flow model which involves deliberate suppression of inherent instabilities of the flow and is formulated, as a linear problem, in terms of the combined contributions of two independent uncorrelated quadrupole-type ring sources, the one convecting in the primary flow representing the sources generated due to the interaction at the primary/secondary interface and the other convecting in the secondary flow representing the sources generated due to the interaction at the secondary/ambient interface. The analysis shows that the effects of flight induce (1) amplication of noise in the forward quadrant, (2) reduction of noise in the aft quadrant and (3) absolutely no impact on radiation of noise at Theta = 90 deg to the jet axis.
Document ID
19830008967
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dash, R.
(Stanford Univ. CA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1982
Subject Category
Acoustics
Report/Patent Number
NASA-CR-169737
SU-JIAA-TR-48-PT-1
NAS 1.26:169737
Report Number: NASA-CR-169737
Report Number: SU-JIAA-TR-48-PT-1
Report Number: NAS 1.26:169737
Accession Number
83N17238
Funding Number(s)
CONTRACT_GRANT: NCC2-75
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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