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Multi-Step Ice Accretion Simulation Using the Level-Set Method
Technical Paper
2019-01-1955
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
Ice accumulation in aircraft is modelled using the Level-Set (LS) method. Current two-dimensional and three-dimensional icing models are limited regarding complex re-meshing due to ice accretion. The Level-Set method allows fully multi-step simulation of ice accretion. The solid boundary is treated implicitly or explicitly. The solid body can be defined via a characteristic level set function in the former case, and as a layer or list of points in the later. Consequently, the boundary conditions for the airflow are applied through a penalization term, or by direct forcing. Correspondingly, the droplet transport is computed using an Eulerian approach in an Immersed Boundary Method (IBM) coupled with Level-Set (IBM-LS) framework, in which the droplet fields impinge on an explicit layer of cells defined by the LS function using a discrete IBM formulation of the interface.
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Al-Kebsi, A., Mose, R., and Hoarau, Y., "Multi-Step Ice Accretion Simulation Using the Level-Set Method," SAE Technical Paper 2019-01-1955, 2019, https://doi.org/10.4271/2019-01-1955.Also In
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