NASA NTRS · 19880001801
Thermal barrier coating life prediction model development
Abstract
This program focuses on predicting the lives of two types of strain-tolerant and oxidation-resistant thermal barrier coating (TBC) systems that are produced by commercial coating suppliers to the gas turbine industry. The plasma-sprayed TBC system is composed of a low pressure, plasma sprayed applied, oxidation resistant NiCrAlY bond coating. The other system is an air plasma sprayed yttria (8 percent) partially stabilized zirconia insulative layer.
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Strangman, T. E., Neumann, J. F., Tasooji, A.. 1985-10-01. Thermal barrier coating life prediction model development. https://ntrs.nasa.gov/citations/19880001801
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