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

Author:

Wang BoyiORCID,Wu YingchunORCID,Zhang LetianORCID,Huang XinyuanORCID,Guo XiangdongORCID,Song XiaomingORCID,Bai PengboORCID,Shi PanORCID,Zhu ShiminORCID,Zhang QianORCID,Liu KaiORCID,Wu XuechengORCID

Abstract

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.

Funder

Aero Engine Corporation of China

Natural Science Foundation of Zhejiang Province

National Natural Science Foundation of China

National Key Research and Development Program of China

Publisher

AIP Publishing

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