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Elastic Moduli and Damping of Vibrational Modes of Aluminum/Silicon Carbide Composite BeamsElastic and shear moduli were determined for two aluminum matrix composites containing 20 and 40 volume percent discontinuous silicon carbide, respectively, using transverse, longitudinal, and torsional vibrational modes of specimens prepared as thin beams. These moduli are consistent with those determined from stress-strain measurements. The damping factors for these modes were also determined. Thermal properties are used to show that part of the damping of transverse modes is caused by the transverse thermal currents discussed by C. Zener (thermo-elastic damping); this damping is frequency-dependent with a maximum damping factor of approximately 0.002. The remaining damping is frequency-independent, and has roughly similar values in transverse, longitudinal, and torsional modes: approximately 0.0001.
Document ID
19960015944
Acquisition Source
Goddard Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Leidecker, Henning
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Subject Category
Composite Materials
Report/Patent Number
Rept-96B00026
NAS 1.15:104626
NASA-TM-104626
Report Number: Rept-96B00026
Report Number: NAS 1.15:104626
Report Number: NASA-TM-104626
Accession Number
96N22135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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