The general problem of calculating the flow fields associated with hypersonic airbreathing aircraft is presented. Unique aspects of hypersonic aircraft aerodynamics are introduced and their demands on computational fluid dynamics are outlined. Example calculations associated with inlet/forebody integration and hypersonic nozzle design are presented to illustrate the nature of the problems considered.


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    Titel :

    Computational analysis of hypersonic airbreathing aircraft flow fields


    Beteiligte:
    Dwoyer, Douglas L. (Autor:in) / Kumar, Ajay (Autor:in)


    Erscheinungsdatum :

    1987-03-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :





    Key technology for airbreathing hypersonic aircraft.

    Nagel, A. L. / Becker, J. V. | NTRS | 1973


    Key technology for airbreathing hypersonic aircraft

    NAGEL, A. / BECKER, J. | AIAA | 1973