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Noise-Path Measurements in Aircraft StructuresSystem determines amount of radiated sound power separately attributed to airborne and structure-borne paths in aircraft. Also used to evaluate vibrating plates and thin shells. Sound transducers include array of lightweight, miniature piezoelectric accelerometers and two-microphone probe. Multichannel Fast Fourier Transform (FFT) analyzer/computer used for analog-to-digital conversion and to analyze spectrum of each of input signals. Noise-path identification in aircraft performed in flight by this system.
Document ID
19850000529
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mcgary, M. C.
Mayes, W. H.
Date Acquired
August 12, 2013
Publication Date
March 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 9
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13017
ISSN: 0145-319X
Report Number: LAR-13017
Accession Number
85B10529
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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