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    Titel :

    Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics


    Beteiligte:

    Kongress:

    32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference



    Erscheinungsdatum :

    01.01.2016




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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