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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 accessioned2026-02-17T21:34:18Z
date available2026-02-17T21:34:18Z
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/4310287
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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