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    Titel :

    Study of slanted perforated shapes in tabs for control of subsonic Jets


    Beteiligte:

    Kongress:

    33rd AIAA Applied Aerodynamics Conference



    Erscheinungsdatum :

    01.01.2015




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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