VSAERO, a subsonic panel method, has grown from a maximum of 1000 panels (unknowns) to the routine use of 10000 panels to model aircraft such as an MD-11 with deployed slats and flaps. The increasing complexity required improvements in user-friendliness including: a robust flow solver; graphical interfaces to generate input and visualize output; algorithms which produce correct results (within the assumptions of potential flow); diagnostics to signal when the assumptions are violated; increased versatility with body wakes and jet exhausts; and multiple ways of generating a model.


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    Titel :

    Subsonic Panel Methods - Second (Order) Thoughts


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    World Aviation Congress & Exposition ; 1998



    Erscheinungsdatum :

    28.09.1998




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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