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    Titel :

    Cross Section Controllable Hypersonic Inlet Design Using Streamline-Tracing and Osculating Axisymmetric Concepts AIAA Paper



    Kongress:

    43rd, Joint propulsion conference ; 2007 ; Cincinnati, OH



    Erscheinungsdatum :

    2007-01-01


    Format / Umfang :

    3373 pages


    Anmerkungen:

    Papers in the range 2007 5004 to 5862. Held on CD-ROM


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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