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    Titel :

    PRELIMINARY DESIGN AND COMPUTATIONAL ANALYSIS OF AN EJECTOR NOZZLE WITH CHEVRONS



    Kongress:

    49th, Aerospace sciences meeting; 49th AIAA Aerospace Sciences meeting including the New Horizons Forum and Aerospace Exposition 2011 ; 2011 ; Orlando, FL



    Erscheinungsdatum :

    01.01.2011


    Format / Umfang :

    17 pages


    Anmerkungen:

    Includes bibliographical references and index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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