Geodesic
The icing process of an aircraft: drop dynamics and wetted surface
Matematičeskoe modelirovanie, Tome 13 (2001) no. 6, pp. 81-86 Cet article a éte moissonné depuis la source Math-Net.Ru

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Dynamics of water droplets of various size in the vicinity of the leading edge of an airfoil is investigated. Bending of drop trajectories (and, consequently, the extention of a wetted wing surface) is shown to depend significantly on the drop deformation and Saffman force, arising in the boundary layer. (Influence of a “near-surface force” caused by the “drop imaginary reflection” is far less). A maximum in the dependence of wetted surface extention on the initial drop radius is revealed. Hence, air viscosity, drop deformation and its break-down in front of a flying apparatus are really important for the following icing process. 
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     author = {A. L. Stasenko and V. A. Tolstykh and D. A. Shirobokov},
     title = {The icing process of an aircraft: drop dynamics and wetted surface},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {81--86},
     year = {2001},
     volume = {13},
     number = {6},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_2001_13_6_a12/}
}
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A. L. Stasenko; V. A. Tolstykh; D. A. Shirobokov. The icing process of an aircraft: drop dynamics and wetted surface. Matematičeskoe modelirovanie, Tome 13 (2001) no. 6, pp. 81-86. http://geodesic.mathdoc.fr/item/MM_2001_13_6_a12/