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

    Film Cooling Performances Under Various Upstream Roughness Conditions: Experimental Investigations and Similarity Hypothesis

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 011::page 111009-1
    Author:
    Huang, Weichen
    ,
    Wang, Kechen
    ,
    Zeng, Fei
    ,
    Chen, Wenbin
    ,
    Zhou, Wenwu
    ,
    Wen, Xin
    ,
    Peng, Di
    ,
    Liu, Yingzheng
    DOI: 10.1115/1.4065682
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Roughness caused by deposition, erosion, and additive manufacturing can significantly affect gas turbine efficiency. Previous research has often examined film cooling performance under limited roughness configurations, resulting in inconclusive findings. In this study, film cooling performances under various upstream roughness conditions were investigated to simulate the roughness-affected film cooling performance of the suction side and the endwall. Three roughness heights (k/D = 0.1, 0.2, and 0.4) and shapes (ks/k = 0.17, 0.67, and 1.95) were selected to cover a wide range of surface roughness characteristics. Three blowing ratios were examined (M = 0.5, 1.0, and 1.5). The weakly roughened surfaces (ks /k = 0.17) showed improved cooling effectiveness as k/D increased. Meanwhile, the moderately and severely roughened surfaces (ks /k = 0.67 and 1.95) showed a decrease in cooling effectiveness with increasing k/D at M = 0.5 and 1.0 but an increase at M = 1.5. Cases with shallower and higher roughness elements at M = 1.5 outperformed the smooth plate. Subsequently, a similarity hypothesis for film cooling effectiveness was proposed. At all blowing ratios, the scaled cooling effectiveness profiles converged around the smooth plate results for ks /D < 0.391, encompassing common turbine roughness scales, including irregularly roughened surfaces. Deviations emerged at ks /D = 0.782, and they were correlated with the deteriorated regions observed at various blowing ratios. Ensemble-averaged scaled cooling effectiveness exponentially grew with increasing roughness scale for all blowing ratios, and an empirical expression based on the smooth plate result and roughness scale was proposed (R2 > 0.97). Finally, the experimental results and fitting correlations of cooling effectiveness were compared. The results demonstrated that the proposed similarity hypothesis potentially facilitated the fast prediction of the roughness-affected film cooling performance.
    • Download: (1.598Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Price: 5000 Rial
    • Statistics

      Film Cooling Performances Under Various Upstream Roughness Conditions: Experimental Investigations and Similarity Hypothesis

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4302647
    Collections
    • Journal of Turbomachinery

    Show full item record

    contributor authorHuang, Weichen
    contributor authorWang, Kechen
    contributor authorZeng, Fei
    contributor authorChen, Wenbin
    contributor authorZhou, Wenwu
    contributor authorWen, Xin
    contributor authorPeng, Di
    contributor authorLiu, Yingzheng
    date accessioned2024-12-24T18:44:04Z
    date available2024-12-24T18:44:04Z
    date copyright6/18/2024 12:00:00 AM
    date issued2024
    identifier issn0889-504X
    identifier otherturbo_146_11_111009.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302647
    description abstractRoughness caused by deposition, erosion, and additive manufacturing can significantly affect gas turbine efficiency. Previous research has often examined film cooling performance under limited roughness configurations, resulting in inconclusive findings. In this study, film cooling performances under various upstream roughness conditions were investigated to simulate the roughness-affected film cooling performance of the suction side and the endwall. Three roughness heights (k/D = 0.1, 0.2, and 0.4) and shapes (ks/k = 0.17, 0.67, and 1.95) were selected to cover a wide range of surface roughness characteristics. Three blowing ratios were examined (M = 0.5, 1.0, and 1.5). The weakly roughened surfaces (ks /k = 0.17) showed improved cooling effectiveness as k/D increased. Meanwhile, the moderately and severely roughened surfaces (ks /k = 0.67 and 1.95) showed a decrease in cooling effectiveness with increasing k/D at M = 0.5 and 1.0 but an increase at M = 1.5. Cases with shallower and higher roughness elements at M = 1.5 outperformed the smooth plate. Subsequently, a similarity hypothesis for film cooling effectiveness was proposed. At all blowing ratios, the scaled cooling effectiveness profiles converged around the smooth plate results for ks /D < 0.391, encompassing common turbine roughness scales, including irregularly roughened surfaces. Deviations emerged at ks /D = 0.782, and they were correlated with the deteriorated regions observed at various blowing ratios. Ensemble-averaged scaled cooling effectiveness exponentially grew with increasing roughness scale for all blowing ratios, and an empirical expression based on the smooth plate result and roughness scale was proposed (R2 > 0.97). Finally, the experimental results and fitting correlations of cooling effectiveness were compared. The results demonstrated that the proposed similarity hypothesis potentially facilitated the fast prediction of the roughness-affected film cooling performance.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFilm Cooling Performances Under Various Upstream Roughness Conditions: Experimental Investigations and Similarity Hypothesis
    typeJournal Paper
    journal volume146
    journal issue11
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4065682
    journal fristpage111009-1
    journal lastpage111009-14
    page14
    treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 011
    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