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Effect of Load Rate on Ultimate Tensile Strength of Ceramic Matrix Composites at Elevated TemperaturesThe strengths of three continuous fiber-reinforced ceramic composites, including SiC/CAS-II, SiC/MAS-5 and SiC/SiC, were determined as a function of test rate in air at 1100 to 1200 C. All three composite materials exhibited a strong dependency of strength on test rate, similar to the behavior observed in many advanced monolithic ceramics at elevated temperatures. The application of the preloading technique as well as the prediction of life from one loading configuration (constant stress-rate) to another (constant stress loading) suggested that the overall macroscopic failure mechanism of the composites would be the one governed by a power-law type of damage evolution/accumulation, analogous to slow crack growth commonly observed in advanced monolithic ceramics. It was further found that constant stress-rate testing could be used as an alternative to life prediction test methodology even for composite materials, at least for short range of lifetimes and when ultimate strength is used as the failure criterion.
Document ID
20020012646
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Choi, Sung R.
(Ohio Aerospace Inst. Brook Park, OH United States)
Gyekenyesi, John P.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
November 1, 2001
Subject Category
Nonmetallic Materials
Report/Patent Number
NASA/TM-2001-211125
E-12975
NAS 1.15:211125
Funding Number(s)
PROJECT: RTOP 714-04-30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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