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Recent advances concerning an understanding of sound transmission through engine nozzles and jetsExperiments on the interaction between a turbulent jet and pure tone sound coming from inside the jet nozzle are reported. This is a model representing the sound transmission from sound sources in jet engines through the nozzle and the jet flow into the far field. It is shown that pure tone sound at low frequencies is considerably attenuated by the jet flow, whereas it is conserved at higher frequencies. On the other hand, broadband jet noise can be amplified considerably by a pure tone excitation. Both effects seem not to be interdependent. Knowledge on how they are created and on relevant parameter dependences allow new considerations for the development of sound attenuators.
Document ID
19780024871
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bechert, D.
(NASA Headquarters Washington, DC United States)
Michel, U.
(NASA Headquarters Washington, DC United States)
Dfizenmaier, E.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1978
Subject Category
Acoustics
Report/Patent Number
PAPER-77-48
NASA-TM-75454
Report Number: PAPER-77-48
Report Number: NASA-TM-75454
Accession Number
78N32814
Funding Number(s)
CONTRACT_GRANT: NASW-3199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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