Published November 25, 1993 | Version public
Journal Article

X-ray residual stress analysis of a ceramic thermal barrier coating undergoing thermal cycling

Abstract

The residual stress of a ZrO_2-8%Y_2O_3 thermal barrier coating was determined as a function of thermal cycling. Samples were thermally cycled from 400°C to 1000°C in air. After a few cycles the samples exhibited a value of compressive residual stress consistent with that determined by considering the thermal expansion coefficients of the coating and substrate. Stress relief occurs in the ZrO_2-Y_2O_3 coating, increasing in both frequency and magnitude with increasing number of thermal cycles. This behavior is explained in terms of a model of failure of coatings in compression.

Additional Information

Copyright © 1993 Elsevier. (Received February 1, 1993; accepted May 14, 1993). The authors gratefully acknowledge the support of the National Science Foundation under Grant No. HRD-9023629. All specimens for this work were provided by the General Electric Company, Aircraft Engine Business Group, Evendale, OH.

Additional details

Identifiers

Eprint ID
49433
Resolver ID
CaltechAUTHORS:20140908-181328570

Funding

NSF
HRD-9023629

Dates

Created
2014-09-10
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Updated
2021-11-10
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