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    Titel :

    Pressure Characteristics of an Aerospike Nozzle in a Rotating Detonation Engine (AIAA 2018-4968)


    Beteiligte:

    Kongress:

    Joint propulsion conference



    Erscheinungsdatum :

    01.01.2018


    Format / Umfang :

    16 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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