Development of a second generation in-flight icing simulation code
BEAUGENDRE, Héloïse
Institut de Mathématiques de Bordeaux [IMB]
Modélisation, contrôle et calcul [MC2]
CFD Lab [Montréal]
Institut de Mathématiques de Bordeaux [IMB]
Modélisation, contrôle et calcul [MC2]
CFD Lab [Montréal]
BEAUGENDRE, Héloïse
Institut de Mathématiques de Bordeaux [IMB]
Modélisation, contrôle et calcul [MC2]
CFD Lab [Montréal]
< Reduce
Institut de Mathématiques de Bordeaux [IMB]
Modélisation, contrôle et calcul [MC2]
CFD Lab [Montréal]
Language
en
Article de revue
This item was published in
Journal of Fluids Engineering. 2006, vol. 128, n° 2, p. 378-387
American Society of Mechanical Engineers
English Abstract
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 ...Read more >
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.Read less <
English Keywords
Ducted fan engine
Helicopter
Helicopter rotor
Ice
Geometrical shape
Aerofoil
Icing
Numerical simulation
Modeling
Computation code
Airplane
Aircraft
Three dimensional flow
Origin
Hal imported