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    Titel :

    Inlet / Body Integration Preliminary Design for Supersonic Air-Breathing Missiles Using Automated Multi-Disciplinary Optimization



    Kongress:

    Symposium, Aerodynamic design and optimisation of flight vehicles in a concurrent multi-disciplinary environment ; 1999 ; Ottawa



    Erscheinungsdatum :

    01.01.2000


    Format / Umfang :

    31 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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