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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Publication date :

    1998


    Size :

    193 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English