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

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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Publication Details

Journal
Journal of Turbomachinery
Published
2025-03-18
DOI
https://doi.org/10.1115/1.4068227
Citations
3
Primary Topic
Laser-induced spectroscopy and plasma
Type
article
Field-Weighted Citation Impact
2.59
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article

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

Junjie Chen, Rui Deng, Jinfeng Peng, Li Shi et al.
3 citations
Journal of Turbomachinery
Laser-induced spectroscopy and plasma
2.59
article

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

Junjie Chen, Rui Deng, Jinfeng Peng, Li Shi, Liang Su, Xiao Tan, Jiasheng Song
article en
3 citations

Abstract

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%.

Journal of TurbomachineryVol. 147(10)
Xiangtan University (CN)
Openalex Percentile: Top 12%
Laser-induced spectroscopy and plasma
2.59
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