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Evaluation of the NASA Ames no. 1 7 by 10 foot wind tunnel as an acoustic test facilityMeasurements were made in the no. 1 7'x10' wind tunnel at NASA Ames Research Center, with the objectives of defining the acoustic characteristics and recommending minimum cost treatments so that the tunnel can be converted into an acoustic research facility. The results indicate that the noise levels in the test section are due to (a) noise generation in the test section, associated with the presence of solid bodies such as the pitot tube, and (b) propagation of acoustic energy from the fan. A criterion for noise levels in the test section is recommended, based on low-noise microphone support systems. Noise control methods required to meet the criterion include removal of hardware items for the test section and diffuser, improved design of microphone supports, and installation of acoustic treatment in the settling chamber and diffuser.
Document ID
19750017896
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilby, J. F.
(Bolt, Beranek, and Newman, Inc. Canoga Park, CA, United States)
Scharton, T. D.
(Bolt, Beranek, and Newman, Inc. Canoga Park, CA, United States)
Date Acquired
September 3, 2013
Publication Date
June 30, 1975
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-137712
BBN-2936
Report Number: NASA-CR-137712
Report Number: BBN-2936
Accession Number
75N25968
Funding Number(s)
CONTRACT_GRANT: NAS2-8382
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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