YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    •   YE&T Library
    • ASME
    • Journal of Turbomachinery
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 009::page 91012-1
    Author:
    Yang, Xing
    ,
    Hao, Zihan
    ,
    Feng, Zhenping
    DOI: 10.1115/1.4067636
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Thermal design for the trailing edge of a turbine vane is critically challenging because the thinnest trailing-edge region has a low-thermal capacity, resulting in a much quicker thermal response to the hot gas. Cooling air for this region is usually extracted from the internal cooling passages inside the vane main body and thus the post-cooling air has a relatively weaker cooling potential. The thermal mismatch in the metal can be further exacerbated by the deposition of fine contaminant particulates resulting from the intake air as well as the unburned hydrocarbon fuel. Changes of the surface conditions caused by deposition are able to affect film cooling and to enhance heat transfer substantially. However, the deposition layer has low-thermal conductivity (approximately 0.1 W · m−1 · K−1), which thermally insulates the wall from the hot gas. The presence of deposition thereby further complicates the heat convection and conduction issues in this area. The current study had the uniqueness of evaluating deposition effects on vane trailing-edge film cooling by conducting deposition simulation experiments, where a scaled-up vane model featured cutback slots with a thick lip on the pressure surface. The coupling effects of deposition and the slot discharge coolant were investigated by examining the dynamic evolution of deposition and flow mixing of the coolant with the mainstream flows for various slot discharge ratios. The resulting film cooling performance was further assessed in adiabatic and conjugate heat transfer conditions to document the deposition-induced changes of heat/mass transfer and conduction. The thick slot lip and higher discharge ratios were found to reduce deposition, but simultaneously, to generate stronger flow mixing. Deposition on the pressure-surface degraded adiabatic cooling effectiveness regardless of deposition thickness, with a maximum reduction of 35%, whereas thicker deposition on the cutback surface was favorable to film cooling at the highest discharge ratio. The insulation effects of the deposition layer were not able to erase out the reduction in adiabatic effectiveness and potentially increased heat transfer levels over the rough deposition surface, resulting in lower overall cooling effectiveness. The reduction in overall effectiveness, however, was alleviated by increasing the discharge ratio.
    • Download: (7.460Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Influences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4305699
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorYang, Xing
    contributor authorHao, Zihan
    contributor authorFeng, Zhenping
    date accessioned2025-04-21T10:12:06Z
    date available2025-04-21T10:12:06Z
    date copyright2/17/2025 12:00:00 AM
    date issued2025
    identifier issn0889-504X
    identifier otherturbo-24-1019.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4305699
    description abstractThermal design for the trailing edge of a turbine vane is critically challenging because the thinnest trailing-edge region has a low-thermal capacity, resulting in a much quicker thermal response to the hot gas. Cooling air for this region is usually extracted from the internal cooling passages inside the vane main body and thus the post-cooling air has a relatively weaker cooling potential. The thermal mismatch in the metal can be further exacerbated by the deposition of fine contaminant particulates resulting from the intake air as well as the unburned hydrocarbon fuel. Changes of the surface conditions caused by deposition are able to affect film cooling and to enhance heat transfer substantially. However, the deposition layer has low-thermal conductivity (approximately 0.1 W · m−1 · K−1), which thermally insulates the wall from the hot gas. The presence of deposition thereby further complicates the heat convection and conduction issues in this area. The current study had the uniqueness of evaluating deposition effects on vane trailing-edge film cooling by conducting deposition simulation experiments, where a scaled-up vane model featured cutback slots with a thick lip on the pressure surface. The coupling effects of deposition and the slot discharge coolant were investigated by examining the dynamic evolution of deposition and flow mixing of the coolant with the mainstream flows for various slot discharge ratios. The resulting film cooling performance was further assessed in adiabatic and conjugate heat transfer conditions to document the deposition-induced changes of heat/mass transfer and conduction. The thick slot lip and higher discharge ratios were found to reduce deposition, but simultaneously, to generate stronger flow mixing. Deposition on the pressure-surface degraded adiabatic cooling effectiveness regardless of deposition thickness, with a maximum reduction of 35%, whereas thicker deposition on the cutback surface was favorable to film cooling at the highest discharge ratio. The insulation effects of the deposition layer were not able to erase out the reduction in adiabatic effectiveness and potentially increased heat transfer levels over the rough deposition surface, resulting in lower overall cooling effectiveness. The reduction in overall effectiveness, however, was alleviated by increasing the discharge ratio.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInfluences of Particulate Deposition on Vane Trailing-Edge Film Cooling: Adiabatic and Overall Cooling Effectiveness
    typeJournal Paper
    journal volume147
    journal issue9
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4067636
    journal fristpage91012-1
    journal lastpage91012-42
    page42
    treeJournal of Turbomachinery:;2025:;volume( 147 ):;issue: 009
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian