Experimental analysis of ice crystal size-velocity correlation in icing wind tunnel with digital holographic particle tracking velocimetry

被引:1
|
作者
Wang, Boyi [1 ]
Wu, Yingchun [1 ]
Zhang, Letian [1 ]
Huang, Xinyuan [1 ]
Guo, Xiangdong [1 ,2 ]
Song, Xiaoming [3 ]
Bai, Pengbo [3 ]
Shi, Pan [3 ]
Zhu, Shimin [4 ]
Zhang, Qian [4 ]
Liu, Kai [4 ]
Wu, Xuecheng [1 ]
机构
[1] Zhejiang Univ, State Key Lab Clean Energy Utilizat, Hangzhou 310027, Peoples R China
[2] China Aerodynam Res & Dev Ctr, Key Lab Icing & Anti Deicing, Mianyang 621000, Peoples R China
[3] AVIC CAPDI Integrat Equipment Co Ltd, Beijing 102206, Peoples R China
[4] AVIC Chengdu CAIC Elect Co LTD, Chengdu 610091, Peoples R China
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
44;
D O I
10.1063/5.0216718
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The ice crystal icing in aero-engines poses a significant threat to aircraft flight safety, and investigating the correlation between ice crystal size and velocity in icing wind tunnels is essential for correlating ground tests with flight conditions. In this paper, a digital holographic particle tracking velocimetry system is developed and integrated with an icing wind tunnel, and the ice crystal size and velocity are simultaneously measured in experiments at four different wind speeds. The velocity difference between the ice crystal and wind has been experimentally observed, and it increases with both the ice crystal size and wind speed. The normalized velocities of the ice crystals by the wind speeds decrease with size, and the maximum velocity difference in the experiments reaches 28% of the wind speed. Additionally, quantitative correlations between ice crystal size and normalized velocity based on the power function and polynomial model are established. The relationship between the particle Reynolds number of ice crystal and size is also analyzed, resulting in the development of a model based on the power function, and the power index ranges from 1.51 to 1.64. These findings will provide valuable assistance in the calibration and commissioning of the ice crystal simulation system in icing wind tunnels, as well as in exploring the correlation between ground icing tests and flight and in developing corresponding models.
引用
收藏
页数:13
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