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Surface protectionThe surface protection subproject consists of three major thrusts: airfoil deposition model; metallic coating life prediction; and thermal barrier coating (TBC) life prediction. The time frame for each of these thrusts and the expected outputs are presented. Further details are given for each thrust such as specific element schedules and the status of performance; in-house, via grant, or via contract.
Document ID
19870001749
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Levine, S. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1984
Publication Information
Publication: Turbine Engine Hot Section Technology, 1984
Subject Category
Metallic Materials
Accession Number
87N11182
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19870001747Collected WorksTurbine Engine Hot Section Technology, 1984
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