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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Supersonic laminar flow development in a square duct


    Contributors:

    Published in:

    Publication date :

    1987-01-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    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. | NTRS | 1987


    Experiments on supersonic turbulent flow development in a square duct

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


    Experiments on supersonic turbulent flow development in a square duct

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