An overview of the Aeroelastic Design Optimization Program (ADOP) at the Douglas Aircraft Company is given. A pilot test program involving the animation of mode shapes with solid rendering as well as wire frame displays, a complete aircraft model of a high-altitude hypersonic aircraft to test ADOP procedures, a flap model, and an aero-mesh modeler for doublet lattice aerodynamics are discussed.


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    Titel :

    Meeting the Challenges with the Douglas Aircraft Company Aeroelastic Design Optimization Program (ADOP)


    Beteiligte:
    B. A. Rommel (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch