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Fatigue damage growth mechanisms in continuous fiber reinforced titanium matrix compositesThe role of fiber/matrix interface strength, residual thermal stresses, and fiber and matrix properties on fatigue damage accumulation in continuous fiber metal matrix composites (MMC) will be discussed. Results from titanium matrix/silicon-carbide fiber composites will be the primary topic of discussion. Results have been obtained from both notched and unnotched specimens at room and elevated temperatures. The stress in the 0 deg fibers has been indentified as the controlling factor in fatigue life. Fatigue of the notched specimens indicated that cracks can grow many fiber spacings in the matrix materials without breaking fibers.
Document ID
19920037102
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Johnson, W. S.
(NASA Langley Research Center Hampton, VA, United States)
Naik, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Pollock, W. D.
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Meeting Information
Meeting: Fatigue 90: International Conference on Fatigue and Fatigue Thresholds
Location: Honolulu, HI
Country: United States
Start Date: July 15, 1990
End Date: July 20, 1990
Accession Number
92A19726
Distribution Limits
Public
Copyright
Other

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