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    Titel :

    VISUALIZATION OF UNSTEADY BEHAVIOR OF SHOCK WAVES AROUND SUPERSONIC INTAKE INSTALLED IN SHOCK TUNNEL



    Kongress:

    Congress; 28th, International Council of the Aeronautical Sciences; ICAS 2010 proceedings ; 2012 ; Brisbane, Australia



    Erscheinungsdatum :

    2012-01-01


    Format / Umfang :

    ICAS2012-P4.5


    Anmerkungen:

    Includes bibliographical references and author index; Held in e-store (RMS)



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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