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Thermal barrier coating life prediction model developmentThe objective is to develop an integrated life prediction model accounting for all potential life-limiting thermal barrier coating (TBC) degradation and failure modes, including spallation resulting from cyclic thermal stress, oxidation degradation, hot corrosion, erosion and foreign object damage.
Document ID
19880001803
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Demasi, J. T. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Sheffler, K. D. (Pratt and Whitney Aircraft East Hartford, CT, 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
88N11185
Funding Number(s)
CONTRACT_GRANT: NAS3-23944
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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