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A research program to reduce interior noise in general aviation airplanes: Investigation of the characteristics of an acoustic panel test facilitySound pressure levels in the test facility were studied that are caused by varying: (1) microphone positions; (2) equalizer setting; and (3) panel clamping forces. Measurements were done by using a Beranek tube or this Beranek tube in combinations with an extension tube and a special test section. In all configurations tests were executed with and without a test panel installed. The influence of the speaker back panel and the back panel of the Beranek tube on the sound pressure levels inside the test tube were also investigated. It is shown that the definition of noise reduction is more useful in relation to this test facility than transmission loss.
Document ID
19780023931
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Grosveld, F.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Vanaken, J.
(Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1978
Subject Category
Acoustics
Report/Patent Number
NASA-CR-157587
KU-FRL-317-9
Report Number: NASA-CR-157587
Report Number: KU-FRL-317-9
Accession Number
78N31874
Funding Number(s)
CONTRACT_GRANT: NSG-1301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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