Progress Toward 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 109(4), 448-451 (Oct 01, 1987) (4 pages) doi:10.1115/1.3240062 History: Received December 01, 1986; Online October 15, 2009


Progress toward developing life models for simulating the behavior of thermal barrier coatings in aircraft gas turbine engines is discussed. A preliminary laboratory model is described as are current efforts to develop engine-capable models. Current understanding into failure mechanisms is also summarized.

Copyright © 1987 by ASME
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