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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Computational analysis of hypersonic airbreathing aircraft flow fields


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


    Erscheinungsdatum :

    01.03.1987


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :





    Computational fluid dynamics for hypersonic airbreathing aircraft

    Thomas, James L. / Dwoyer, Douglas L. / Kumar, Ajay | NTRS | 1991