Morphogenetic modelling of in-flight icing

Details Morphogenetic modelling of in-flight icing Morphogenetic modelling of in-flight icing

G - Physics

06

F

G06F 19/00 (2011.01) B64D 15/20 (2006.01) G06F 17/10 (2006.01)

Patent

CA 2430823

The accretion of ice on an aerodynamic surface is predicted by identifying predetermined atmospheric parameters relevant to ice formation in a particular fluid environment. Then the behaviour of individual fluid elements is simulated based on the identified parameters to create a model of the ice accretion.

L'accrétion de glace sur une surface aérodynamique est prédite en identifiant des paramètres atmosphériques prédéterminés, pertinents pour la formation de glace dans un environnement fluide en particulier. Le comportement des éléments fluides individuels est ensuite simulé en se basant sur les paramètres identifiés afin de créer un modèle d'accrétion de la glace.

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