BEAUGENDRE, Héloïse; MORENCY, François; HABASHI, W. G.

Métadonnées

Licence d’utilisation du document

BEAUGENDRE, Héloïse
Institut de Mathématiques de Bordeaux [IMB]
Modélisation, contrôle et calcul [MC2]
CFD Lab [Montréal]

MORENCY, François
CFD Lab [Montréal]

HABASHI, W. G.
CFD Lab [Montréal]

Langue

Article de revue

Ce document a été publié dans

Journal of Fluids Engineering. 2006, vol. 128, n° 2, p. 378-387

American Society of Mechanical Engineers

Résumé en anglais

Two-dimensional and quasi-3D in-flight ice accretion simulation codes have been widely used by the aerospace industry for the last two decades as an aid to the certification process. The present paper proposes an efficient numerical method for calculating ice shapes on simple or complex 3D geometries. The resulting ice simulation system, FENSAP-ICE, is built in a modular fashion to successively solve each flow, impingement and accretion via field models based on partial differential equations (PDEs). The FENSAP-ICE system results are compared to other numerical and experimental results on 2D and slightly complex 3D geometries. It is concluded that FENSAP-ICE gives results in agreement with other code calculation results, for the geometries available in the open literature.< Réduire

Mots clés en anglais

Ducted fan engine

Helicopter

Helicopter rotor

Ice

Geometrical shape

Aerofoil

Icing

Numerical simulation

Modeling

Computation code

Airplane

Aircraft

Three dimensional flow

Origine

Importé de hal

Unités de recherche

Institut de Mathématiques de Bordeaux (IMB) - UMR 5251