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    Title :

    DUAL-BELL NOZZLE FOR SPACE LAUNCHERS WITH FLUIDIC CONTROL OF TRANSITION


    Contributors:

    Conference:

    AIAA Propulsion and Energy Forum ; 2021 ; Online


    Published in:

    Publication date :

    2021



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    52.30 Strömungskraftmaschinen, Turbomaschinen / 55.60 Raumfahrttechnik



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    Control of Space Launchers

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    Dual-Bell Nozzle Design

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