28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-2.6.1
NUMERICAL METHOD FOR ICE ACCRETION ON 3D WINGS
J. M. Hospers, H. W. M. Hoeijmakers
Univ. of Twente, Netherlands
Keywords: icing, multi-phase, splashing, cfd, eulerian
To numerically calculate ice accretion shapes on 3D wings the numerical method Droplerian was developed, using an Eulerian method. The method is intended for SLD conditions. The 2D method has been extended to 3D and was compared to experimental impingement data and to the previous two dimensional results.
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