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    Titel :

    A Computational Study of Hypersonic Boundary Layer Stability on a Blunt Nose Flared Cone Model



    Kongress:

    29th Joint propulsion conference ; 1993 ; Monterey; CA



    Erscheinungsdatum :

    01.01.1993


    Format / Umfang :

    AIAA 93-3486


    Anmerkungen:

    Separate paper nos 93-1752 to 93-4557 with gaps held only


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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