Modeling of Ice Accretion on the Airfoil Surface in an Air Flow Containing Ice Particles
- Authors: Kashevarov A.V.1, Stasenko A.L.1,2
-
Affiliations:
- Central Aerohydrodynamic Institute named after N. E. Zhukovsky
- Moscow Institute of Physics and Technology
- Issue: Vol 59, No 4 (2018)
- Pages: 645-652
- Section: Article
- URL: https://journals.rcsi.science/0021-8944/article/view/161195
- DOI: https://doi.org/10.1134/S0021894418040107
- ID: 161195
Cite item
Abstract
The process of airfoil icing caused by incidence of ice crystals is considered. A physicomathematical model of motion of spheroidal crystals in the gas flow and their interaction with the body is formulated. The model takes into account the non-spherical particle orientation with respect to the velocity vector of the gas flow. It is assumed that the particle impact onto the body surface leads to partial destruction of the particle under the action of normal and tangential stresses, and some part of the particle mass remains in the vicinity of the impact point. An inviscid flow around the airfoil with a time-dependent shape is calculated by the method of approximate conformal mapping.
About the authors
A. V. Kashevarov
Central Aerohydrodynamic Institute named after N. E. Zhukovsky
Author for correspondence.
Email: a.v.kash@yandex.ru
Russian Federation, Zhukovsky, 140180
A. L. Stasenko
Central Aerohydrodynamic Institute named after N. E. Zhukovsky; Moscow Institute of Physics and Technology
Email: a.v.kash@yandex.ru
Russian Federation, Zhukovsky, 140180; Zhukovsky, 140180
Supplementary files
