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contributor authorS. M. Meier
contributor authorT. A. Cruse
contributor authorD. M. Nissley
contributor authorK. D. Sheffler
date accessioned2017-05-08T23:38:26Z
date available2017-05-08T23:38:26Z
date copyrightApril, 1992
date issued1992
identifier issn1528-8919
identifier otherJETPEZ-26699#258_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/110233
description abstractA thermal barrier coated (TBC) turbine component design system, including an accurate TBC life prediction model, is needed to realize the full potential of available TBC engine performance and/or durability benefits. The objective of this work, which was sponsored in part by NASA under the Hot Section Technology (HOST) Program (Contract NAS3-23944), was to generate a life prediction model for electron beam-physical vapor deposited (EB-PVD) zirconia TBC. Specific results include EB-PVD zirconia mechanical and physical properties, coating adherence strength measurements, interfacial oxide growth characteristics, quantitative cyclic thermal spallation life data, and a spallation life model.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermal Barrier Coating Life Prediction Model Development
typeJournal Paper
journal volume114
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906581
journal fristpage258
journal lastpage263
identifier eissn0742-4795
keywordsElectrons
keywordsVapors
keywordsCoating processes
keywordsCoatings
keywordsMeasurement
keywordsEngines
keywordsSpallation (Nuclear physics)
keywordsDesign
keywordsDurability
keywordsTurbine components
keywordsModel development AND Thermal barrier coatings
treeJournal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 002
contenttypeFulltext


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