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Investigation of the sonic fatigue characteristics of randomly excited aluminum viscoelastic panels at ambient temperaturesSonic fatigue effects on structural reliability of randomly excited aluminum viscoelastic panels at ambient temperatures
Document ID
19660012407
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Moskal, B. J. (North American Aviation, Inc. Columbus, OH, United States)
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-425
Report Number: NASA-CR-425
Accession Number
66N21696
Funding Number(s)
CONTRACT_GRANT: NAS1-4728
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SOUND INTENSITY
ALUMINUM
PANEL
STRUCTURAL FATIGUE

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