Recent work on the analysis of iced airfoils and wings is described. Ice shapes for multielement airfoils and wings are computed using an extension of the LEWICE code that was developed for single airfoils. The aerodynamic properties of the iced wing are determined with an interactive scheme in which the solutions of the inviscid flow equations are obtained from a panel method and the solutions of the viscous flow equations are obtained from an inverse three-dimensional finite-difference boundary-layer method. A new interaction law is used to couple the inviscid and viscous flow solutions. The newly developed LEWICE multielement code is amplified to a high-lift configuration to calculate the ice shapes on the slat and on the main airfoil and on a four-element airfoil. The application of the LEWICE wing code to the calculation of ice shapes on a MS-317 swept wing shows good agreement with measurements. The interactive boundary-layer method is applied to a tapered iced wing in order to study the effect of icing on the aerodynamic properties of the wing at several angles of attack.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Recent progress in the analysis of iced airfoils and wings


    Contributors:


    Publication date :

    1992-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Analysis of iced wings

    CEBECI, TUNCER / CHEN, H. / KAUPS, K. et al. | AIAA | 1992


    Detached Eddy Simulations for Iced Airfoils

    Pan, J. | Online Contents | 2005


    Calculation of Flow Over Iced Airfoils

    Tuncer Cebeci | AIAA | 1989


    SmaggIce: Further Progress in Software for Gridding 2D Iced Airfoils

    Vickerman, Mary / Choo, Yung / Schilling, Herbert et al. | AIAA | 2005


    Detached Eddy Simulations for Iced Airfoils

    Jianping Pan / Eric Loth | AIAA | 2005