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내부냉각노즐의 열차폐코팅을 위한 복합열전달 해석기법 연구Study on the Conjugate Heat Transfer Analysis Methodology of Thermal Barrier Coating on the Internal Cooled Nozzle

Other Titles
Study on the Conjugate Heat Transfer Analysis Methodology of Thermal Barrier Coating on the Internal Cooled Nozzle
Authors
김인겸김진욱이동호조진수
Issue Date
Jun-2015
Publisher
한국유체기계학회
Keywords
Thermal barrier coating(열차폐코팅); Internal cooled nozzle(내부냉각노즐); Conjugate heat transfer(복합열전달); Computational fluid dynamics(전산유체역학)
Citation
한국유체기계학회 논문집, v.18, no.3, pp 38 - 45
Pages
8
Indexed
KCI
Journal Title
한국유체기계학회 논문집
Volume
18
Number
3
Start Page
38
End Page
45
URI
https://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/202453
DOI
10.5293/kfma.2015.18.3.038
ISSN
2287-9706
Abstract
In this study, two computational methodologies were compared to consider an effective conjugate heat transfer analysis technique for the cooled vane with thermal barrier coating. The first one is the physical modeling method of the TBC layer on the vane surface, which means solid volume of the TBC on the vane surface. The second one is the numerical modeling method of the TBC layer by putting the heat resistance interface condition on the surface between the fluid and solid domains, which means no physical layer on the vane surface. For those two methodologies, conjugate heat transfer analyses were conducted for the cooled vane with TBC layer having various thickness from 0.1 mm to 0.3 mm. Static pressure distributions for two cases show quite similar patterns in the overall region while the physical modeling shows quite a little difference around the throat area. Thermal analyses indicated that the metal temperature distributions are quite similar for both methods. The results show that the numerical modeling method can reduce the computational resources significantly and is quite suitable method to evaluate the overall performance of TBC even though it does not reflect the exact geometry and flow field characteristics on the vane surface.
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