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Significance of thermal contact resistance in two-layer thermal-barrier-coated turbine vanesThe importance of thermal contact resistance between layers in heat transfer through two layer, plasma sprayed, thermal barrier coatings applied to turbine vanes was investigated. Results obtained with a system of NiCrAlY bond and yttria stabilized zirconia ceramic show that thermal contact resistance between layers is negligible. These results also verified other studies which showed that thermal contact resistance is negligible for a different coating system of NiCr bond calcia stabilized zirconia ceramic. The zirconia stabilized ceramic thermal conductivity data scatter presented in the literature is ?20 to -10 percent about a curve fit of the data. More accurate predictions of heat transfer and metal wall temperatures are obtained when the thermal conductivity values are used at the ?20 percent level.
Document ID
19800014821
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Liebert, C. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Gaugler, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-420
NASA-TM-81483
Meeting Information
Meeting: Intern Conf. on Met. Coatings
Location: San Diego, CA
Country: United States
Start Date: April 21, 1980
End Date: April 25, 1980
Sponsors: Am. Vacuum Soc.
Accession Number
80N23310
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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