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Acousto-ultrasonic decay in metal matrix composite panelsAcousto-ultrasonic (A-U) decay rates (UD) were measured in metal matrix composite (MMC) panels. The MMC panels had fiber architectures and cross-sectional thicknesses corresponding to those designed for aerospace turbine engine structures. The wavelength-to-thickness ratio produced by the combination of experimental frequency setting conditions and specimen geometry was found to be a key parameter for identifying optimum conditions for UD measurements. The ratio was shown to be a useful rule of thumb when applied to ceramic matrix composites (CMC)s and monolithic thermo-plastics.
Document ID
19960009436
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kautz, Harold E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Subject Category
Quality Assurance And Reliability
Report/Patent Number
NASA-TM-106972
E-9733
NAS 1.15:106972
Report Number: NASA-TM-106972
Report Number: E-9733
Report Number: NAS 1.15:106972
Accession Number
96N16602
Funding Number(s)
PROJECT: RTOP 510-01-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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