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High Temperature Tensile Properties and Fatigue Behavior of a Melt-Infiltrated SiC/SiC CompositeHigh temperature fatigue behavior of a woven, SiC/SiC ceramic matrix composite (CMC) was investigated in air at two temperatures. The reinforcement for the CMC consisted of 5HS Sylramic(Trademark) fabric with a [0deg/90deg]4s lay-up. The SiC matrix material was infiltrated into the fiber-preform with a slurry-cast, melt-infiltration process. Tensile and fatigue test specimens were machined from the CMC plates. Initially tensile tests were conducted to obtain the average values of tensile properties at 1038 and 1204 C. Subsequently, low-cycle fatigue (LCF) tests with zero and two-hour hold-times at the maximum stress were conducted at the same two temperatures. Fatigue life data generated in the LCF tests were used to determine the geometric mean fatigue lives. In this paper, the tensile behavior and the fatigue durability of the CMC determined under different loading conditions are documented. In addition, reductions observed in the cyclic lives of the composite due to the two hour hold-time at maximum tensile stress are discussed.
Document ID
20020073442
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kalluri, Sreeramesh
(Ohio Aerospace Inst. Cleveland, OH United States)
Calomino, Anthony M.
(NASA Glenn Research Center Cleveland, OH United States)
Brewer, David N.
(Army Research Lab. Brook Park, OH United States)
Kiraly, Louis J.
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Composite Materials
Meeting Information
Meeting: Fatigue 202: 8th International Fatigue Congress
Location: Stockholm
Country: Sweden
Start Date: June 2, 2002
End Date: June 7, 2002
Sponsors: EMAS
Funding Number(s)
CONTRACT_GRANT: NCC3-618
PROJECT: RTOP 714-04-30
Distribution Limits
Public
Copyright
Public Use Permitted.
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