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A directional microphone array for acoustic studies of wind tunnel modelsAn end-fire microphone array that utilizes a digital time delay system has been designed and evaluated for measuring noise in wind tunnels. The directional response of both a four- and eight-element linear array of microphones has enabled substantial rejection of background noise and reverberations in the NASA Ames 40- by 80-foot wind tunnel. In addition, it is estimated that four- and eight-element arrays reject 6 and 9 dB, respectively, of microphone wind noise, as compared with a conventional omnidirectional microphone with nose cone. Array response to two types of jet engine models in the wind tunnel is presented. Comparisons of array response to loudspeakers in the wind tunnel and in free field are made.
Document ID
19740052654
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Soderman, P. T.
(NASA Ames Research Center Moffett Field, Calif., United States)
Noble, S. C.
(U.S. Army, Air Mobility R & D Laboratory, Moffett Field Calif., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1974
Subject Category
Facilities, Research, And Support
Report/Patent Number
AIAA PAPER 74-640
Meeting Information
Meeting: Aerodynamic Testing Conference
Location: Bethesda, MD
Start Date: July 8, 1974
End Date: July 10, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A35404
Distribution Limits
Public
Copyright
Other

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