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Publishing Language: Chinese

Experiment on critical fragmentation velocity of partially melted ice particles impacting a rigid surface

Zonghui LIU1,2Xueqin BU1Jiayi BAO1( )Guiping LIN2
School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China
Hangzhou International Innovation Institute, Beihang University, Hangzhou 311115, China
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Abstract

The problem of ice crystal icing seriously affects the flight safety of aircraft, and the impact behavior of partially melted ice particles is the key to the study of engine icing. A high-speed impact test rig for partially melted ice particles was designed and constructed, and a heat transfer based ice crystal melting rate measurement method was used and calibrated. Partially melted ice particle impact experiments were conducted at different diameters, impact velocities, and melting rates, and the effect of liquid water on critical fragmentation was discussed in terms of the ice particle fragmentation model. Further, a relative water film thickness coefficient θ is defined to scale the effect of the presence of liquid water on the impact fragmentation of partially melted ice crystals, and an experimental correlation equation for the critical fragmentation velocity of partially melted ice crystals is obtained based on the experimental data. This study improved the understanding of the impact crushing mechanism of partially melted ice particles, and provided a certain theoretical basis for the impact model and the adhesion model of partially melted ice crystals.

CLC number: V21 Document code: A Article ID: 1000-6893(2025)14-131558-11

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
LIU Z, BU X, BAO J, et al. Experiment on critical fragmentation velocity of partially melted ice particles impacting a rigid surface. Acta Aeronautica et Astronautica Sinica, 2025, 46(14). https://doi.org/10.7527/S1000-6893.2025.31558

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Received: 21 November 2024
Revised: 16 December 2024
Accepted: 20 February 2025
Published: 27 April 2025
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica