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NASA NTRS · 20030001874

Transient Reliability of Ceramic Structures For Heat Engine Applications

Abstract

The objectives of this report was to develop a methodology to predict the time-dependent reliability (probability of failure) of brittle material components subjected to transient thermomechanical loading, taking into account the change in material response with time. This methodology for computing the transient reliability in ceramic components subjected to fluctuation thermomechanical loading was developed, assuming SCG (Slow Crack Growth) as the delayed mode of failure. It takes into account the effect of varying Weibull modulus and materials with time. It was also coded into a beta version of NASA's CARES/Life code, and an example demonstrating its viability was presented.

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BibTeXRIS

Nemeth, Noel N., Jadaan, Osama M.. 2002-10-01. Transient Reliability of Ceramic Structures For Heat Engine Applications. https://ntrs.nasa.gov/citations/20030001874

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