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    Titel :

    Integration Methodology for Waverider-Derived Hypersonic Inlet and Vehicle Forebody (AIAA 2014-3229)


    Beteiligte:

    Kongress:

    19th, AIAA international space planes and hypersonic systems and technologies conference ; 2014 ; Atlanta, GA



    Erscheinungsdatum :

    01.01.2014


    Format / Umfang :

    12 pages


    Anmerkungen:

    Includes bibliographical references and author index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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