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Off axis loading of silicon carbide fibers in a titanium aluminide matrixSilicon carbide SCS-6 fibers in a Ti24A1 + 11Nb matrix were subjected to off axis loading in a 'thin-slice' pushout test, resulting in various combinations of shear, radial compression, and tension along the fibers as a function of orientation angle. The load necessary for debonding decreased as the orientation angle increased, whereas the average frictional sliding stress after 60 s of sliding remained relatively constant for orientation angles less than 30 deg. Analyses of the specimen bending stresses and of the contact stresses by finite element modeling and thin plate theory are presented.
Document ID
19950028427
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Kennefick, C. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: Acta Metallurgica et Materialia
Volume: 41
Issue: 10
ISSN: 0956-7151
Subject Category
Composite Materials
Accession Number
95A60026
Distribution Limits
Public
Copyright
Other

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