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.


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    Title :

    Simulation of Ice Accretion on Airfoils during Flight


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

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



    Publication date :

    2003-06-16




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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