The use of parametric flow analysis, rather than parametric scale testing, to support the design of an ejector system offers a number of potential advantages. The application of available 3-D flow analyses to the design ejectors can be subdivided into several key elements. These are numerics, turbulence modeling, data handling and display, and testing in support of analysis development. Experimental and predicted jet exhaust for the Boeing 727 aircraft are examined.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Numerical prediction of 3-D ejector flows


    Beteiligte:
    Roberts, D. W. (Autor:in) / Paynter, G. C. (Autor:in)


    Erscheinungsdatum :

    1979-09-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Numerical simulation of transient flows in a vacuum ejector-diffuser system

    Lijo, V / Kim, H D / Rajesh, G et al. | SAGE Publications | 2010



    EFFECTS OF MULTIPLE PRIMARY FLOWS ON EJECTOR PERFORMANCE IN AN EJECTOR-RAM ROCKET ENGINE

    Gregory, D. C. / Han, S. / AIAA | British Library Conference Proceedings | 2003


    Numerical simulation of ejector rocket flow

    Velazquez, A. / Matesanz, A. / Tizon, J. et al. | AIAA | 1998