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Thermal barrier coating life prediction model developmentThis 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.
Document ID
19880001801
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Strangman, T. E. (Garrett Turbine Engine Co. Phoenix, AZ, United States)
Neumann, J. F. (Garrett Turbine Engine Co. Phoenix, AZ, United States)
Tasooji, A. (Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Publication Information
Publication: NASA. Lewis Research Center, Turbine Engine Hot Section Technology, 1985
Subject Category
Mechanical Engineering
Accession Number
88N11183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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