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Progress toward life modeling of thermal barrier coatings for aircraft gas turbine enginesProgress toward developing life models for simulating the behavior of thermal barrier coatings in aircraffft gas turbine engines is discussed. A preliminary laboratory model is described as are current efforts to develop engine-capable models. Current understanding of failure mechanisms is also summarized.
Document ID
19880027893
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Miller, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1987
Publication Information
Publication: ASME, Transactions, Journal of Engineering for Gas Turbines and Power
Volume: 109
ISSN: 0022-0825
Subject Category
Nonmetallic Materials
Report/Patent Number
ASME PAPER 87-ICE-18
Accession Number
88A15120
Distribution Limits
Public
Copyright
Other

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