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    Titel :

    Pressure Sensitive Paint Application to a Wing-Body Model in a Hypersonic Shock Tunnel


    Beteiligte:

    Kongress:

    22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ; 2002 ; St. Louis , Missouri



    Erscheinungsdatum :

    01.01.2002




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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