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Investigation of Cooling Performances of a Non-Film-Cooled Turbine Vane Coated with a Thermal Barrier Coating Using Conjugate Heat Transfer
Prapamonthon P; Yooyen S; Sleesongsom S; Dipasquale D; Xu HZ; Wang JH; Ke ZQ
Source PublicationENERGIES
2018-04-01
Volume11Issue:4
ISSN1996-1073
AbstractThe aim of this paper is to numerically investigate cooling performances of a non-film-cooled turbine vane coated with a thermal barrier coating (TBC) at two turbulence intensities (Tu = 8.3% and 16.6%). Computational fluid dynamics (CFD) with conjugate heat transfer (CHT) analysis is used to predict the surface heat transfer coefficient, overall and TBC effectiveness, as well as internal and average temperatures under a condition of a NASA report provided by Hylton et al. [NASA CR-168015]. The following interesting phenomena are observed: (1) At each Tu, the TBC slightly dampens the heat transfer coefficient in general, and results in the quantitative increment of overall cooling effectiveness about 16-20%, but about 8% at the trailing edge (TE). (2) The protective ability of the TBC increases with Tu in many regions, that is, the leading edge (LE) and its neighborhoods on the suction side (SS), as well as the region from the LE to the front of the TE on the pressure side (PS), because the TBC causes the lower enhancement of the heat transfer coefficient in general at the higher Tu. (3) Considering the internal and average temperatures of the vane coated with two different TBCs, although the vane with the lower thermal conductivity protects more effectively, its role in the TE region reduces more significantly. (4) For both TBCs, the increment of Tu has a relatively small effect on the reduction of the average temperature of the vane.
KeywordTurbine Vane Heat Transfer Coefficient Thermal Barrier Coating Turbulence Intensity Conjugate Heat Transfer
DOI10.3390/en11041000
Indexed BySCI ; EI
Language英语
WOS IDWOS:000434703400311
WOS KeywordFREESTREAM TURBULENCE
WOS Research AreaEnergy & Fuels
WOS SubjectEnergy & Fuels
Funding OrganizationNatural Science Foundation of China(51376168) ; King Mongkut's Institute of Technology Ladkrabang
Classification二类
Ranking1
Citation statistics
Cited Times:1[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/77509
Collection流固耦合系统力学重点实验室
Recommended Citation
GB/T 7714
Prapamonthon P,Yooyen S,Sleesongsom S,et al. Investigation of Cooling Performances of a Non-Film-Cooled Turbine Vane Coated with a Thermal Barrier Coating Using Conjugate Heat Transfer[J]. ENERGIES,2018,11(4).
APA Prapamonthon P.,Yooyen S.,Sleesongsom S.,Dipasquale D.,Xu HZ.,...&Ke ZQ.(2018).Investigation of Cooling Performances of a Non-Film-Cooled Turbine Vane Coated with a Thermal Barrier Coating Using Conjugate Heat Transfer.ENERGIES,11(4).
MLA Prapamonthon P,et al."Investigation of Cooling Performances of a Non-Film-Cooled Turbine Vane Coated with a Thermal Barrier Coating Using Conjugate Heat Transfer".ENERGIES 11.4(2018).
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