The main objectives of the research was to further develop the necessary fundamental algorithms to enable high fidelity multi-disciplinary design of complete aircraft configurations. The work was focused on four main areas: (1) Flow solution algorithms for unstructured meshes, (2) Aero-structural plan-form optimization, (3) Multi-fidelity approach to multi-disciplinary design of supersonic aircraft. (4) Algorithms for automatic feedback control of aerodynamic flows.


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    Title :

    High-Fidelity Multidisciplinary Design Using an Integrated Design Environment


    Contributors:
    A. Jameson (author)

    Publication date :

    2007


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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