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    Titel :

    NUMERICAL SIMULATION OF FLOW THROUGH SCRAMJET INLET - ISOLATOR MODEL WITH COOLING AND GEOMETRICAL MODIFICATIONS


    Beteiligte:

    Kongress:

    AIAA International Space Planes and Hypersonic Systems and Technologies Conference ; 23. ; 2020 ; Montréal



    Erscheinungsdatum :

    2020


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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