The numerical simulation of flows around complex aircraft configurations like the Fokker 50 and Fokker 100, is described. In these simulations multiblock grids and a 3D Euler-flow solver are used. The major features of the grid-generation procedure and flow solver are outlined. Results of the validation of the numerical-flow-simulation system for aerodynamic design work are presented.


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    Titel :

    3D Euler Flows around Modern Airplanes


    Beteiligte:

    Erscheinungsdatum :

    1989


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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