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    Titel :

    Experiments on Shock-Boundary Layer Interaction and Cooling Efficiency in a Transpiration Cooled Model Scramjet (AIAA 2017-4833)


    Beteiligte:

    Kongress:

    Joint propulsion conference



    Erscheinungsdatum :

    01.01.2017


    Format / Umfang :

    18 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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