A numerical finite-volume method is proposed for solving the Euler equations of a steady three-dimensional flow. The subsonic regions embedded in steady supersonic flow about aircraft are computed by introducing a time-dependent coordinate system that maps the fuselage and wing into one coordinate surface. The suitability of the method to a delta-winged aircraft is demonstrated, and its applicability to rectangular-winged aircraft and problems in internal transonic flow is pointed out.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Finite-volume solution of the Euler equations for steady three-dimensional transonic flow


    Beteiligte:
    Rizzi, A. (Autor:in) / Bailey, H. (Autor:in)

    Kongress:

    International Conference on Numerical Methods in Fluid Dynamics ; 1976 ; Enschede, Netherlands


    Erscheinungsdatum :

    01.01.1976


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Finite-volume solutions to the Euler equations in transonic flow

    SCHMIDT, W. / JAMESON, A. / WHITFIELD, D. | AIAA | 1981


    Finite-Volume Solutions to the Euler Equations in Transonic Flow

    Wolfgang Schmidt / Antony Jamesont / David Whitfield | AIAA | 1983