A simplified, uncoupled zonal procedure was utilized to assess the capability of numerically simulating icing effects on a Boeing 727-200 aircraft. The computational approach combines potential flow, plus boundary layer simulations by VSAERO for the un-iced aircraft forces and moments, with Navier-Stokes simulations by ARC3D for the incremental forces and moments due to iced components. These are compared with wind tunnel longitudinal force and moment data. Although the computational results compared favorably with the test data in the linear angle of attack range, it is clear that for general aircraft icing calculations, a multiblock Navier-Stokes code will be required for the viscous component of this zonal method.


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    Titel :

    CFD zonal modeling of leading-edge ice effects for a complete aircraft


    Beteiligte:
    Summa, J. M. (Autor:in) / Strash, D. J. (Autor:in) / Lednicer, D. A. (Autor:in)

    Kongress:

    AIAA, Aerospace Sciences Meeting and Exhibit ; 1993 ; Reno, NV, United States


    Erscheinungsdatum :

    1993-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    CFD zonal modeling of leading-edge ice effects for a complete aircraft

    SUMMA, J. / STRASH, D. / LEDNICER, D. | AIAA | 1993


    Improved CFD Zonal Modeling of Leading-Edge Ice Effects for a Complete Aircraft

    Strash, D. J. / Summa, J. M. / AIAA | British Library Conference Proceedings | 1994



    Improved CFD Zonal Modeling of Leading-Edge Ice Effects for a Complete Aircraft

    Strash, D. J. / Summa, J. M. / AIAA | British Library Conference Proceedings | 1994


    AIRCRAFT LEADING EDGE ASSEMBLY

    GAO JUN / WU ZHIBIN / KONG LINGYONG et al. | Europäisches Patentamt | 2022

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