Oxidation-Based Model for Thermal Barrier Coating Life

Author:

MILLER ROBERT A.

Publisher

Wiley

Subject

Materials Chemistry,Ceramics and Composites

Reference10 articles.

1. 1R. A. Miller, S.R. Levine, and S. Stecura , "Thermal Barrier Coatings for Aircraft Gas Turbines ," American Institute of Aeronautics and Astronautics paper AIAA-80-302, 1980 .

2. 2T. A. Taylor, M. O. Price, and R. O. Tucker , "Response of Plasma Sprayed MgO-ZrO2and ZrO2-6.6 Y2O3to Thermal Fatigue and Hot Corrosion " pp.6 -131 in Proceedings of the Second Conference on Advanced Materials for Alternate-Fuel-Capable Heat Engines, EPRI RD-2369-SR, 1982 .

3. 3S. Duvall , "Processing Technology for Advanced Metallic and Ceramic Turbine Airfoil Coatings " pp.6 -102 in Proceeding s of the Second Conference on Advanced Materials for Alternate-Fuel-Capable Heat Engines, EPRI RD-2369-SR, 1982 .

4. 4T. E. Strangman , "Thermal Barrier Coatings for Turbine Airfoils ,"; to be published inThin Solid Films.

5. Failure mechanisms of thermal barrier coatings exposed to elevated temperatures

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