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    Titel :

    Closed-Loop Control of Shock Location in Mach 1.8 Direct Connect Wind Tunnel (AIAA 2014-2935)


    Beteiligte:

    Kongress:

    Conference; 7th, Flow control; 7th AIAA flow control conference 2014; Atlanta, Georgia, USA, 16-20 June 2014 : held at the AIAA aviation forum 2014 ; 2014 ; Atlanta, GA



    Erscheinungsdatum :

    2014-01-01


    Format / Umfang :

    13 pages


    Anmerkungen:

    Includes bibliographical references and index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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