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    Titel :

    Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-off Distance


    Beteiligte:

    Kongress:

    16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference



    Erscheinungsdatum :

    2009-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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