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dc.contributor.authorShi, Li
dc.contributor.authorTan, Xiao
dc.contributor.authorDeng, Rongli
dc.contributor.authorSu, Liang
dc.contributor.authorPeng, Jinfeng
dc.contributor.authorSong, Jiasheng
dc.contributor.authorChen, Junjie
dc.date.accessioned2026-02-17T21:34:18Z
dc.date.available2026-02-17T21:34:18Z
dc.date.copyright4/8/2025 12:00:00 AM
dc.date.issued2025
dc.identifier.issn0889-504X
dc.identifier.otherturbo-24-1282.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4310287
dc.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%.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleAn Unsteady Deposition Model for Evaluating CMAS Nonuniform Deposition Behavior and Aerodynamic Performance Degradation Under Hot Streak Clocking Effect
dc.typeJournal Paper
dc.journal.volume147
dc.journal.issue10
dc.journal.titleJournal of Turbomachinery
dc.identifier.doi10.1115/1.4068227
dc.journal.fristpage101012-1
dc.journal.lastpage101012-15
dc.page15
dc.treeJournal of Turbomachinery:;2025:;volume( 147 ):;issue: 010
dc.contenttypeFulltext


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