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NASA NTRS ยท 19850028159

Oxidation-based model for thermal barrier coating life

Abstract

A procedure is described for modeling the lives of thermal barrier coatings subjected to high-temperatrue environments. The models is used to calculate cycles-to-failure as a function of heating cycle duration. It is based on the presumption that oxidation is the single important time-dependent factor which limits the life of these coatings, and that oxidation-induced strains combine with cyclic strains to promote slow crack growth in the ceramic layer. Good agreement is obtained between calculated and experimental lives for specimens tested in a furnace. This shows that an oxidation-based approach is promising. The importance of reproducible specimen preparation is also discussed.

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BibTeXRIS

Miller, R. A.. 1984-08-01. Oxidation-based model for thermal barrier coating life. https://ntrs.nasa.gov/citations/19850028159

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