Aligned with the needs of the aeronautics industry the general aim of the UFAST project is to foster experimental and theoretical work in the highly non-linear area of unsteady shock wave boundary layer interaction (SWBLI). Although in the past several EU projects were aiming at transonic/supersonic flows, the area of unsteady shock wave boundary layer interaction has not yet been treated. Moreover, experimental methods as well as numerical approaches have been improved considerably.


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    Title :

    UFAST Project - Unsteady Effects in Shock Wave Induced Separation


    Contributors:


    Publication date :

    2010


    Size :

    3 Seiten





    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English