Life Modeling of Thermal Barrier Coatings for Aircraft Gas Turbine Engines
- 1 April 1989
- journal article
- Published by ASME International in Journal of Engineering for Gas Turbines and Power
- Vol. 111 (2) , 301-305
- https://doi.org/10.1115/1.3240251
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.Keywords
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