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The effect of temperature on the deformation and fracture of SiC/Ti-24Al-11NbThe effect of temperature on the stress-strain behavior in air and the failure mechanisms of Ti-24Al-11Nb alloy and of a SiC/Ti-24Al-11Nb composite with continuous SiC fibers oriented parallel to the loading direction was investigated over temperature range 23-815 C. It was found that the tensile failure process of SiC/Ti-24Al-11Nb was controlled at all temperatures by fiber fracture. Composite failure occurred at 0.8 percent strain at all temperatures. Debond and frictional stresses at the fiber-matrix interface decreased with increased temperature.
Document ID
19920072519
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Brindley, P. K. (NASA Lewis Research Center Cleveland, OH, United States)
Draper, S. L. (NASA Lewis Research Center Cleveland, OH, United States)
Eldridge, J. I. (NASA Lewis Research Center Cleveland, OH, United States)
Nathal, M. V. (NASA Lewis Research Center Cleveland, OH, United States)
Arnold, S. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
September 1, 1992
Publication Information
Publication: Metallurgical Transactions A - Physical Metallurgy and Materials Science
Volume: 23A
Issue: 9, Se
ISSN: 0360-2133
Subject Category
Composite Materials
Report/Patent Number
ISSN: 0360-2133
Accession Number
92A55143
Distribution Limits
Public
Copyright
Other

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