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NASA NTRS · 19880067126

Thermal barrier coating life prediction model development

Abstract

A life prediction model for correlating the spallation life of ceramic thermal barrier coatings is developed which includes both cyclic and time-dependent damage. The cyclic damage is related to the calculated cyclic inelastic strain range, while the time-dependent damage is related to the oxidation kinetics at the bond-ceramic interface. The cyclic inelastic strain range is calculated using a modified form of the Walker viscoplastic material model; calculation of the oxidation kinetics is based on traditional oxidation algorithms using experimentally determined parameters. The correlation between the actual and predicted spallation lives is within a factor of 3.

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Cruse, T. A., Stewart, S. E., Ortiz, M.. 1988-06-01. Thermal barrier coating life prediction model development. https://ntrs.nasa.gov/citations/19880067126

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