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    An Unsteady Deposition Model for Evaluating CMAS Nonuniform Deposition Behavior and Aerodynamic Performance Degradation Under Hot Streak Clocking Effect

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 010::page 101012-1
    Author:
    Shi, Li
    ,
    Tan, Xiao
    ,
    Deng, Rongli
    ,
    Su, Liang
    ,
    Peng, Jinfeng
    ,
    Song, Jiasheng
    ,
    Chen, Junjie
    DOI: 10.1115/1.4068227
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An unsteady model has been developed for evaluating deposition behavior and aerodynamic performance degradation under the impact of hot streak. The results reveal that hot streak alters the force exerted by the mainstream, impacting the impact behavior of particles. For particles of 1 μm, total impact numbers for the uniform inlet case, vane-aligned case, and passage-aligned case are 431, 1244, and 325 on the pressure side. The hot streak clocking effect significantly affects particle temperature and deposit formation. In the vane-aligned case, the deposition mass fraction on the suction side increases from 13.8% in the uniform inlet case to 18.7%, while in the passage-aligned case, it decreases to 5.4%. Furthermore, the hot streak clocking effect leads to increased total pressure losses and a decline in aerodynamic performance, especially in the vane-aligned case. After 4000 h of deposition, the dynamic pressure loss in the vane-aligned case increases from 3.7% in the uniform inlet case to 4.3%.
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      An Unsteady Deposition Model for Evaluating CMAS Nonuniform Deposition Behavior and Aerodynamic Performance Degradation Under Hot Streak Clocking Effect

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4308124
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    • Journal of Turbomachinery

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    contributor authorShi, Li
    contributor authorTan, Xiao
    contributor authorDeng, Rongli
    contributor authorSu, Liang
    contributor authorPeng, Jinfeng
    contributor authorSong, Jiasheng
    contributor authorChen, Junjie
    date accessioned2025-08-20T09:20:47Z
    date available2025-08-20T09:20:47Z
    date copyright4/8/2025 12:00:00 AM
    date issued2025
    identifier issn0889-504X
    identifier otherturbo-24-1282.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4308124
    description abstractAn unsteady model has been developed for evaluating deposition behavior and aerodynamic performance degradation under the impact of hot streak. The results reveal that hot streak alters the force exerted by the mainstream, impacting the impact behavior of particles. For particles of 1 μm, total impact numbers for the uniform inlet case, vane-aligned case, and passage-aligned case are 431, 1244, and 325 on the pressure side. The hot streak clocking effect significantly affects particle temperature and deposit formation. In the vane-aligned case, the deposition mass fraction on the suction side increases from 13.8% in the uniform inlet case to 18.7%, while in the passage-aligned case, it decreases to 5.4%. Furthermore, the hot streak clocking effect leads to increased total pressure losses and a decline in aerodynamic performance, especially in the vane-aligned case. After 4000 h of deposition, the dynamic pressure loss in the vane-aligned case increases from 3.7% in the uniform inlet case to 4.3%.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Unsteady Deposition Model for Evaluating CMAS Nonuniform Deposition Behavior and Aerodynamic Performance Degradation Under Hot Streak Clocking Effect
    typeJournal Paper
    journal volume147
    journal issue10
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4068227
    journal fristpage101012-1
    journal lastpage101012-15
    page15
    treeJournal of Turbomachinery:;2025:;volume( 147 ):;issue: 010
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian