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Thermal barrier coating life-prediction model developmentThe primary objective of this program was to develop an operative thermal barrier coating (TBC) design model for life prediction. The objective was successfully accomplished with the development, calibration, and demonstration of a mechanistic thermochemical model which rapidly predicts TBC life as a function of engine, mission, and materials system parameters. This thermochemical design model accounts for the three operative TBC damage modes (bond coating oxidation, zirconia toughness reduction, and molten salt film damage), which all contribute to spalling of the insulating zirconia layer.
Document ID
19890007960
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Strangman, T. E.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Neumann, J. F.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Liu, A.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA, Lewis Research Center, Turbine Engine Hot Section Technology, 1987
Subject Category
Structural Mechanics
Accession Number
89N17331
Funding Number(s)
CONTRACT_GRANT: NAS3-23945
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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