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RESEARCH PAPERS

Life Modeling of Thermal Barrier Coatings for Aircraft Gas Turbine Engines

[+] Author and Article Information
R. A. Miller

NASA Lewis Research Center, Cleveland, OH 44135

J. Eng. Gas Turbines Power 111(2), 301-305 (Apr 01, 1989) (5 pages) doi:10.1115/1.3240251 History: Received November 17, 1987; Online October 15, 2009

Abstract

Thermal barrier coating life models developed under the NASA Lewis Research Center’s Hot Section Technology (HOST) program are summarized. An initial laboratory model and three design-capable models are discussed. Current understanding of coating failure mechanisms is also summarized.

Copyright © 1989 by ASME
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