In this study, a computational method is presented that computes ice accretion on airfoils in specified icing conditions. A good agreement is found with the ice shapes predicted by other computational methods. Agreement with the experimental ice shapes is fair. Also, the implementation and application of a mathematical model of a thermal anti-icing system in the ice accretion simulation code 2DFOIL-ICE is presented. The numerical code has proved to be able to calculate the main parameters of an airfoil anti-icing system, such as: solid surface temperatures (for the wetted region), runback water flow and convection heat transfer coefficient distributions along the external surface.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Simulation of Ice Accretion on Airfoils during Flight


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    FAA In-flight Icing / Ground De-icing International Conference & Exhibition ; 2003



    Erscheinungsdatum :

    16.06.2003




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Simulation of Ice Accretion on Airfoils during Flight

    Dillingh, J. E. / Hoeijmakers, H. W. M. / SAE et al. | British Library Conference Proceedings | 2003


    Flow and Ice Accretion Simulation around Multiple Airfoils

    Volkers, D. F. / Van Lipzig, N. / De Cock, K. M. J. | British Library Online Contents | 1994


    Flow and Ice Accretion Simulation around Multiple Airfoils

    Volkers, D. F. / Van Lipzig, N. / De Cock, K. M. J. et al. | British Library Conference Proceedings | 1994


    Ice Accretion Prediction on Multielement Airfoils

    Mingione, G. | Online Contents | 1998