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Noise measurement in wind tunnels, workshop summaryIn reviewing the progress made in acoustic measurements in wind tunnels over the 5-yr span of the workshops, it is evident that a great deal of progress has occurred. Specialized facilities are now on line, special measurement techniques were developed, and corrections were devised and proven. This capability is in the process of creating a new and more correct data bank on acoustic phenomena, and represents a major step forward in acoustics technology. Additional work is still required, but now, rather than concentrating on facilities and techniques, researchers may more profitably concentrate on noise-source modeling, with the simulation of propulsor noise source (in flight) and of propulsor/airframe airflow characteristics. Promising developments in directional acoustic receivers and other discrimination/correlation techniques should now be regularly exploited, in part for model noise-source diagnosis, but also to expedite extraction of the lone source signal from any residual background noise and reverberation in the working chamber and from parasitic noise due to essential rigs or instrumentation inside the airstream.
Document ID
19820026312
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hickley, D. H.
(RAE Farnborough, United Kingdom)
Williams, J.
(RAE Farnborough, United Kingdom)
Date Acquired
September 4, 2013
Publication Date
September 1, 1982
Subject Category
Acoustics
Report/Patent Number
A-8843
NASA-TM-84219
NAS 1.15:84219
Report Number: A-8843
Report Number: NASA-TM-84219
Report Number: NAS 1.15:84219
Accession Number
82N34188
Funding Number(s)
PROJECT: RTOP 505-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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