The development of a nozzle which combines the hypermixing and lobe mechanisms to achieve further increases in jet entrainment and ejector performance is investigated. A computer program which incorporates a two equation turbulence model and is used to predict and compare the evolution of jets from various nozzle designs is discussed. Increasing the length of the nozzle lobes and an alternating lobe nozzle are a methods examined for increasing the entrainment rate.


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    Titel :

    Computer aided design study of hypermixing nozzles


    Beteiligte:


    Erscheinungsdatum :

    01.09.1979


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    COMPUTER-AIDED DESIGN STUDY OF HYPERMIXING NOZZLES

    MEFFERD, L.A. / BEVILAQUA, P.M. | AIAA | 1980


    Progress toward synergistic hypermixing nozzles

    DAVIS, D. / HINGST, W. | AIAA | 1991


    Mass entrainment by hypermixing jets

    Salter, G. | Tema Archiv | 1975


    Computer-Aided Design Study of Hypermixing Nozzles

    L. A. Mefferd / P. M. Bevilaqua | NTIS | 1978