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Noise transmission loss of aircraft panels using acoustic intensity methodsThe two-microphone, cross-spectral, acoustic intensity measurement technique was used to determine the acoustic transmission loss of three different aircraft panels. The study was conducted in the transmission loss apparatus in the Langley aircraft noise reduction laboratory.
Document ID
19820023193
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Mcgary, M. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1982
Subject Category
Acoustics
Report/Patent Number
NAS 1.60:2046
L-15306
NASA-TP-2046
Accession Number
82N31069
Funding Number(s)
PROJECT: RTOP 505-33-53-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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