Supersonic laminar flow development in a constant-area square duct exhibits as one of its distinguishing features the formation of two contrarotating secondary flow vortices centered about the corner bisector. This phenomenon does not occur in unbounded corner flow. The secondary flow causes an outward bulging of total pressure contours in the vicinity of the corner bisector for wholly attached flow conditions.


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    Titel :

    Supersonic laminar flow development in a square duct


    Beteiligte:
    Davis, D. O. (Autor:in) / Gessner, F. B. (Autor:in) / Kerlick, G. D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.01.1987



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Supersonic laminar flow development in a square duct

    DAVIS, D. O. / GESSNER, F. B. / KERLICK, G. D. et al. | AIAA | 1987


    Experiments on supersonic turbulent flow development in a square duct

    GESSNER, F. B. / FERGUSON, S. D. / LO, C. H. | AIAA | 1987


    Experiments on supersonic turbulent flow development in a square duct

    Gessner, F. B. / Ferguson, S. D. / Lo, C. H. | NTRS | 1987


    Experiments on supersonic turbulent flow development in a square duct

    GESSNER, F. / FERGUSON, S. / LO, C. | AIAA | 1986