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A procedure for predicting internal and external noise fields of blowdown wind tunnelsThe noise generated during the operation of large blowdown wind tunnels is considered. Noise calculation procedures are given to predict the test-section overall and spectrum level noise caused by both the tunnel burner and turbulent boundary layer. External tunnel noise levels due to the tunnel burner and circular jet exhaust flow are also calculated along with their respective cut-off frequency and spectrum peaks. The predicted values are compared with measured data, and the ability of the prediction procedure to estimate blowdown-wind-tunnel noise levels is shown.
Document ID
19720017059
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hosier, R. N.
(Army Air Mobility R and D Lab. Hampton, VA, United States)
Mayes, W. H.
(NASA Langley Research Center)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Physics, General
Report/Patent Number
NASA-TM-X-2556
L-8132
Report Number: NASA-TM-X-2556
Report Number: L-8132
Accession Number
72N24709
Funding Number(s)
PROJECT: RTOP 132-80-01-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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