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Fracture Strength of Single-Crystal Silicon Carbide Microspecimens at Room and Elevated TemperatureThree shapes of tensile specimens were tested--curved with a very low stress concentration factor and straight with either a circular hole or an elliptical hole. The nominal thickness was 125 micron with a net section 100 micron wide; the overall length of these microspecimens was 3.1 mm. They were fabricated by an improved version of deep reactive ion etching, which produced specimens with smooth sidewalls and cross-sections having a slightly trapezoidal shape that was exaggerated inside the holes. The novel test setup used a vertical load train extending into a resistance furnace. The specimens had wedge-shaped ends which fit into ceramic grips. The fixed grip was mounted on a ceramic post, and the movable grip was connected to a load cell and actuator outside the furnace with a ceramic-encased nichrome wire. The same arrangement was used for tests at 24 and at 1000 C. The strengths of the curved specimens for two batches of material (made with slightly different processes) were 0.66+/-0.12 GPa and 0.45+/-0.20 GPa respectively at 24 C with identical values at 1000 C. The fracture strengths of the circular-hole and elliptical-hole specimens (computed from the stress concentration factors and measured loads at failure) were approximately 1.2 GPa with slight decreases at the higher temperature. Fractographic examinations showed failures initiating on the surface--primarily at corners. Weibull predictions of fracture strengths for the hole specimens based on the properties of the curved specimens were reasonably effective for the circular holes, but not for the elliptical holes.
Document ID
20070034927
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Nemeth, Noel N.
(NASA Glenn Research Center Cleveland, OH, United States)
Sharpe, William N., Jr.
(Johns Hopkins Univ. Baltimore, MD, United States)
Beheim, Glenn M.
(NASA Glenn Research Center Cleveland, OH, United States)
Evans, Laura J.
(NASA Glenn Research Center Cleveland, OH, United States)
Jadaan, Osama M.
(Wisconsin Univ. Platteville, WI, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2007
Subject Category
Mechanical Engineering
Report/Patent Number
E-16167
NASA/TM-2007-214990
Report Number: E-16167
Report Number: NASA/TM-2007-214990
Funding Number(s)
WBS: WBS 984754.02.07.03.19.05
Distribution Limits
Public
Copyright
Public Use Permitted.
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