Experimental Quantization of Droplet Spatial Distribution in Icing Wind Tunnel with HACPI

The cloud spatial uniformity in the test section is crucial for icing wind tunnels in aircraft icing research and airworthiness certification. To achieve uniform supercooled large droplet (SLD) icing conditions, both the spatial variation in droplet size distribution and the concentration should be considered. In this study, the spatial distribution of droplets under three SLD conditions is explored in the Aviation Industry Corporation of China Aerodynamics Research Institute (AVICARI)’s FL-61 icing wind tunnel. Measurements are conducted at 12 test points in vertical and horizontal directions using the holographic airborne cloud particle imager (HACPI) in conjunction with a two-axis traversing system. The droplet images obtained at specific test points below the test section centerline show deformation phenomena for droplets larger than 400 μm. Additionally, the aspect ratio of deformed droplets increases with droplet size. The spatial evolution of the median volume diameter (MVD) and liquid water content (LWC) is examined. For two spray arrangements where the activated nozzles are positioned close, the test point where the LWC peak in the vertical direction occurs is higher than that of the MVD peak. Further analysis focuses on the size distribution of droplets in the vertical direction. The results show that the settling effect of the droplets larger than 50 μm is evident under a flow velocity of 78 m/s. Meanwhile, the position where large droplets tend to appear lowers as the droplet size increases. Finally, the spatial uniformity of droplet size distributions at the same radial distance is discussed.

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Publication Details

Journal
Aerospace
Published
2026-03-15
DOI
https://doi.org/10.3390/aerospace13030274
Primary Topic
Icing and De-icing Technologies
Type
article
Field-Weighted Citation Impact
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article

Experimental Quantization of Droplet Spatial Distribution in Icing Wind Tunnel with HACPI

Xu Wu, Quanzhong Xia, Bohan Wang, Zhiqiang Zhang et al.
Aerospace
Icing and De-icing Technologies
article

Experimental Quantization of Droplet Spatial Distribution in Icing Wind Tunnel with HACPI

Xu Wu, Quanzhong Xia, Bohan Wang, Zhiqiang Zhang, Letian Zhang, Xiangdong Guo, Zhen Liu, Yingchun Wu, Si Li
article en

Abstract

The cloud spatial uniformity in the test section is crucial for icing wind tunnels in aircraft icing research and airworthiness certification. To achieve uniform supercooled large droplet (SLD) icing conditions, both the spatial variation in droplet size distribution and the concentration should be considered. In this study, the spatial distribution of droplets under three SLD conditions is explored in the Aviation Industry Corporation of China Aerodynamics Research Institute (AVICARI)’s FL-61 icing wind tunnel. Measurements are conducted at 12 test points in vertical and horizontal directions using the holographic airborne cloud particle imager (HACPI) in conjunction with a two-axis traversing system. The droplet images obtained at specific test points below the test section centerline show deformation phenomena for droplets larger than 400 μm. Additionally, the aspect ratio of deformed droplets increases with droplet size. The spatial evolution of the median volume diameter (MVD) and liquid water content (LWC) is examined. For two spray arrangements where the activated nozzles are positioned close, the test point where the LWC peak in the vertical direction occurs is higher than that of the MVD peak. Further analysis focuses on the size distribution of droplets in the vertical direction. The results show that the settling effect of the droplets larger than 50 μm is evident under a flow velocity of 78 m/s. Meanwhile, the position where large droplets tend to appear lowers as the droplet size increases. Finally, the spatial uniformity of droplet size distributions at the same radial distance is discussed.

AerospaceVol. 13(3)
China Aerodynamics Research and Development Center (CN), Shanghai Advanced Research Institute (CN), Aero Engine Corporation of China (China) (CN), State Key Laboratory of Clean Energy Utilization, Zhejiang University (CN)
Affordable and clean energy
Openalex Percentile: Top 18%
Icing and De-icing Technologies
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