Computational unsteady aerodynamics (CUA) is a critical element in the prediction of flutter stability and dynamic response of aircraft. Linear aerodynamic methods are still the most widely used, but more advanced methods are receiving increased attention. The purpose of this Workshop was to review methods in use and to give exposure to other methods which are currently available or are in the development process.


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    Titel :

    Numerical Unsteady Aerodynamic and Aeroelastic Simulation (l'Aerodynamique instationnaire numerique et la simulation de l'aeroelasticite)


    Erscheinungsdatum :

    1998


    Format / Umfang :

    193 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch