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Correlation microphone for measuring airframe noise in large-scale wind tunnelsA correlation microphone arrangement was used in the test section of the Ames 7- by 10-Foot and 40- by 80-Foot Wind Tunnels in an attempt to reject the reverberant and wind noise. The tests in the 7- by 10-foot wind tunnel covered a frequency range from 400 Hz to 8 kHz while the tests in the 40- by 80-foot tunnel covered the range from 31.5 to 800 Hz. Examination of the experimental data plus calculations of cross-correlations due to reflective noise indicate that the correlation microphone is effective in rejecting microphone wind noise and reverberant noise even at low frequencies, and that the low-frequency background noise monitored by the correlation microphone is reflected noise with a preferred direction from the tunnel drive system. Design studies indicate that this tunnel drive noise can be reduced substantially through suitable modification of the drive fans and acoustical treatment of the nacelles that house these fans.
Document ID
19760058424
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ahtye, W. F.
(NASA Ames Research Center Moffett Field, CA, United States)
Kojima, G. K.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 76-553
Meeting Information
Meeting: Aero-Acoustics Conference
Location: Palo Alto, CA
Start Date: July 20, 1976
End Date: July 23, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A41390
Distribution Limits
Public
Copyright
Other

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