The present paper deals with the accretion of supercooled large droplets (SLD) at high velocity on wall. A visualization technique of the accretion of ice is used to measure and characterize the thickness of ice during the accretion phenomenon. Influences of air velocity, air temperature, drop size, impact angle and altitude were studied. The experiments are conducted in the ONERA icing wind tunnel, which allows to reach regimes close to realistic conditions for aircrafts (i.e. high velocity: → 190 m/s and altitude: → 11 500 m).
Influence of Realistic Aircraft Conditions on Accretion of Supercooled Large Droplet
Sae Technical Papers
International Conference on Icing of Aircraft, Engines, and Structures ; 2023
15.06.2023
Aufsatz (Konferenz)
Englisch
Influence of Realistic Aircraft Conditions on Accretion of Supercooled Large Droplet
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