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Environmental/Thermal Barrier Coatings for Ceramic Matrix Composites: Thermal Tradeoff StudiesRecent interest in environmental/thermal barrier coatings (EBC/TBCs) has prompted research to develop life-prediction methodologies for the coating systems of advanced high-temperature ceramic matrix composites (CMCs). Heat-transfer analysis of EBC/TBCs for CMCs is an essential part of the effort. It helps establish the resulting thermal profile through the thickness of the CMC that is protected by the EBC/TBC system. This report documents the results of a one-dimensional analysis of an advanced high-temperature CMC system protected with an EBC/TBC system. The one-dimensional analysis was used for tradeoff studies involving parametric variation of the conductivity; the thickness of the EBC/TBCs, bond coat, and CMC substrate; and the cooling requirements. The insight gained from the results will be used to configure a viable EBC/TBC system for CMC liners that meet the desired hot surface, cold surface, and substrate temperature requirements.
Document ID
20070034699
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Murthy, Pappu L. M.
(NASA Glenn Research Center Cleveland, OH, United States)
Brewer, David
(Army Research Lab. Cleveland, OH, United States)
Shah, Ashwin R.
(Sest, Inc. Middleburgh Heights, OH, United States)
Date Acquired
August 24, 2013
Publication Date
July 1, 2007
Subject Category
Composite Materials
Report/Patent Number
E-16142
NASA/TM-2007-214920
Report Number: E-16142
Report Number: NASA/TM-2007-214920
Funding Number(s)
CONTRACT_GRANT: NAS3-26385
CONTRACT_GRANT: NASA Order C-77005-T
WBS: WBS 984754.02.07.03.11.03
CONTRACT_GRANT: NASA Order C-73506-N
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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