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SUMMARY:Numerical simulations of high-speed droplet splashing - Steve Mill
 more\, Laboratory for Scientific Computing\, The Cavendish Laboratory
DTSTART:20140206T160000Z
DTEND:20140206T170000Z
UID:TALK49086@talks.cam.ac.uk
CONTACT:Stephen Walley
DESCRIPTION:Droplet impact on aircraft surfaces at high altitude can lead 
 to ice forming on the leading edge of the aerofoil\, with potentially seri
 ous aerodynamic consequences.  In order to develop improved technology to 
 prevent ice accretion\, detailed understanding of the physical processes w
 ithin the splash is required.  A numerical model to deal with the behaviou
 r of very high speed impact (around 100 m/s) is presented\, incorporating 
 the key physical features required to accurately model droplet splashing i
 n this regime.
LOCATION:Mott Seminar Room\, Cavendish Laboratory
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