The desire to operate rotorcraft in icing conditions has renewed the interest in developing high-fidelity analysis methods to predict ice accumulation and the ensuing rotor performance degradation. A subset of providing solutions for rotorcraft icing problems is predicting two-dimensional ice accumulation on rotor airfoils. While much has been done to predict ice for fixed-wing airfoil sections, the rotorcraft problem has two additional challenges: first, rotor airfoils tend to experience flows in higher Mach number regimes, often creating glaze ice which is harder to predict; second, rotor airfoils oscillate in pitch to produce balance across the rotor disk. A methodology and validation test cases are presented to solve the rotor airfoil problem as an important step to solving the larger rotorcraft icing problem. The process couples Navier-Stokes CFD analysis with the ice accretion analysis code, LEWICE3D. The process is applied to several airfoil cases for which there are experimental data.


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    Titel :

    Calculations of Ice Shapes on Oscillating Airfoils


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Narducci, Robert (Autor:in) / Reinert, Tonja (Autor:in)

    Kongress:

    SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing ; 2011



    Erscheinungsdatum :

    13.06.2011




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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