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contributor authorSun, J. G.
date accessioned2017-05-09T01:09:35Z
date available2017-05-09T01:09:35Z
date issued2014
identifier issn0022-1481
identifier otherht_136_08_081601.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/155340
description abstractThermal properties of thermal barrier coatings (TBCs) are important parameters for the safe and efficient operation of advanced turbine engines. This paper presents a new method, the pulsed thermal imaging–multilayer analysis (PTI–MLA) method, which can measure the coating thermal conductivity and heat capacity distributions over an entire engine component surface. This method utilizes a multilayer heat transfer model to analyze the surface temperature response acquired from a onesided pulsed thermal imaging experiment. It was identified that several experimental system parameters and TBC material parameters may affect the coating surface temperature response. All of these parameters were evaluated and incorporated as necessary into the formulations. The PTI–MLA method was demonstrated by analyzing three TBC samples, and the experimental results were compared with those obtained from other methods.
publisherThe American Society of Mechanical Engineers (ASME)
titlePulsed Thermal Imaging Measurement of Thermal Properties for Thermal Barrier Coatings Based on a Multilayer Heat Transfer Model
typeJournal Paper
journal volume136
journal issue8
journal titleJournal of Heat Transfer
identifier doi10.1115/1.4027551
journal fristpage81601
journal lastpage81601
identifier eissn1528-8943
treeJournal of Heat Transfer:;2014:;volume( 136 ):;issue: 008
contenttypeFulltext


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