Modeling of Ice Accretion on the Airfoil Surface in an Air Flow Containing Ice Particles
- Авторлар: Kashevarov A.V.1, Stasenko A.L.1,2
-
Мекемелер:
- Central Aerohydrodynamic Institute named after N. E. Zhukovsky
- Moscow Institute of Physics and Technology
- Шығарылым: Том 59, № 4 (2018)
- Беттер: 645-652
- Бөлім: Article
- URL: https://journals.rcsi.science/0021-8944/article/view/161195
- DOI: https://doi.org/10.1134/S0021894418040107
- ID: 161195
Дәйексөз келтіру
Аннотация
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.
Негізгі сөздер
Авторлар туралы
A. Kashevarov
Central Aerohydrodynamic Institute named after N. E. Zhukovsky
Хат алмасуға жауапты Автор.
Email: a.v.kash@yandex.ru
Ресей, Zhukovsky, 140180
A. Stasenko
Central Aerohydrodynamic Institute named after N. E. Zhukovsky; Moscow Institute of Physics and Technology
Email: a.v.kash@yandex.ru
Ресей, Zhukovsky, 140180; Zhukovsky, 140180
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