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    Title :

    DESIGN OF SHAPE TRANSITION NOZZLE FOR DIRECT-CONNECT SUPERSONIC COMBUSTOR


    Contributors:

    Conference:

    AIAA Propulsion and Energy Forum ; 2021 ; Online



    Publication date :

    2021



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik




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