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contributor authorY. R. Takeuchi
contributor authorK. Kokini
date accessioned2017-05-08T23:44:18Z
date available2017-05-08T23:44:18Z
date copyrightJanuary, 1994
date issued1994
identifier issn1528-8919
identifier otherJETPEZ-26722#266_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113638
description abstractControlled experiments and a corresponding analytical model were developed to investigate the reasons for crack initiation in multilayer ceramic thermal barrier coatings. The experiments and model determined that surface cracks form as a result of tensile stresses created following stress relaxation in the ceramic at steady-state high temperatures (about 900°C–1100°C). Interface cracks generated by out-of-plane stresses are affected by the presence of these surface cracks and thermal transients and, possibly, edge effects.
publisherThe American Society of Mechanical Engineers (ASME)
titleThermal Fracture of Multilayer Ceramic Thermal Barrier Coatings
typeJournal Paper
journal volume116
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906803
journal fristpage266
journal lastpage271
identifier eissn0742-4795
keywordsCeramics
keywordsFracture (Process)
keywordsThermal barrier coatings
keywordsSurface cracks
keywordsStress
keywordsFracture (Materials)
keywordsRelaxation (Physics)
keywordsTension
keywordsSteady state AND High temperature
treeJournal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 001
contenttypeFulltext


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