Supercooled large droplet (SLD) impact on ice at high velocity : splashing characterization - Archive ouverte HAL
Communication Dans Un Congrès Année : 2022

Supercooled large droplet (SLD) impact on ice at high velocity : splashing characterization

Résumé

The present paper deals with the impact of supercooled large droplets (SLD) at high velocity on walls of different characteristics (smooth/clean substrate vs. rough/iced surface resulting from continuous ice accretion). A visualization technique of the impact is presented to track and observe the splashing event over time. A focus is proposed on the characterization of the re-emitted droplets after the impact, especially on the particle size, velocity and ejection angle distributions. The experiments are conducted in the ONERA icing wind tunnel which allows to reach regimes where the Weber number is of the order of 160 000, which extends the range of velocities usually found in the literature to characterize the impact of SLD.
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Dates et versions

hal-04039717 , version 1 (21-03-2023)

Identifiants

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Thomas Alary, Baptiste Dejean, Pierre Berthoumieu, Pierre Trontin. Supercooled large droplet (SLD) impact on ice at high velocity : splashing characterization. AIAA Aviation 2022 Forum, Jun 2022, Chicago, United States. ⟨10.2514/6.2022-4116⟩. ⟨hal-04039717⟩
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