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The isothermal fatigue behavior of a unidirectional SiC/Ti composite and the Ti alloy matrixThe high temperature fatigue behavior of a metal matrix composite (MMC) consisting of Ti-15V-3Cr-3Al-3Sn (Ti-15-3) matrix reinforced by 33 vol percent of continuous unidirectional SiC fibers was experimentally and analytically evaluated. Isothermal MMC fatigue tests with constant amplitude loading parallel to the fiber direction were performed at 300 and 550 C. Comparative fatigue tests of the Ti-15-3 matrix alloy were also conducted. Composite fatigue behavior and the in-situ stress state of the fiber and matrix were analyzed with a micromechanical model, the Concentric Cylinder Model (CCM). The cyclic stress-strain response of the composite was stable at 300 C. However, an increase in cyclic mean strain foreshortened MMC fatigue life at high strain ranges at 550 C. Fatigue tests of the matrix alloy and CCM analyses indicated this response was associated with stress relaxation of the matrix in the composite.
Document ID
19890013313
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gayda, John, Jr.
(NASA Lewis Research Center Cleveland, OH, United States)
Gabb, Timothy P.
(NASA Lewis Research Center Cleveland, OH, United States)
Freed, Alan D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1989
Subject Category
Composite Materials
Report/Patent Number
E-4683
NASA-TM-101984
NAS 1.15:101984
Report Number: E-4683
Report Number: NASA-TM-101984
Report Number: NAS 1.15:101984
Accession Number
89N22684
Funding Number(s)
PROJECT: RTOP 505-63-1A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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