NASA NTRS · 19890007960
Thermal barrier coating life-prediction model development
Abstract
The 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.
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Strangman, T. E., Neumann, J. F., Liu, A.. 1987-10-01. Thermal barrier coating life-prediction model development. https://ntrs.nasa.gov/citations/19890007960
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