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Evaluation of acoustic emission technique for crack growth measurement in aeronautical structuresAn investigation has been conducted concerning the possibility to use the acoustic emission technique for the measurement of fatigue crack growth in aluminum alloy specimens. Two types of aluminum alloys were tested in the investigation. It was found that the acoustic emission technique provides a reliable indication of changes in the crack dimensions over relatively short periods of time. The level of acoustic activity serves as an indicator of the size of the cracks.
Document ID
19740056434
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Singh, J. J.
Davis, W. T.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Structural Mechanics
Meeting Information
Meeting: International Instrumentation Symposium
Location: Albuquerque, NM
Start Date: May 21, 1974
End Date: May 23, 1974
Accession Number
74A39184
Distribution Limits
Public
Copyright
Other

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