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    Titel :

    Numerical Investigation of High-pressure Combustion in Rocket Engines Using Flamelet/Progress-Variable Models (AIAA 2015-1109)


    Beteiligte:

    Kongress:

    Aerospace sciences meeting



    Erscheinungsdatum :

    01.01.2015


    Format / Umfang :

    16 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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