The final report consists of AIAA papers. The report presents an analytical performance prediction methodology for annular propulsion nozzles with and without swirl introduced in the combustor upstream of the nozzle. Four types of swirlers were investigated: free vortex, constant angle, forced vortex and Rankine vortex swirlers. For the no-swirl case thrust efficiencies and static pressure profiles from cold flow testing of selected nozzles are summarized and compared to the predictions.... Ramjets, Supersonics.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Analytical and Experimental Investigation of Annular Propulsive Nozzles


    Beteiligte:
    R. R. Conley (Autor:in) / J. D. Hoffman (Autor:in) / H. D. Thompson (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    37 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    An analytical and experimental investigation of annular propulsive nozzles

    CONLEY, R. R. / HOFFMAN, J. D. / THOMPSON, H. D. | AIAA | 1985


    An analytical and experimental investigation of annular propulsive nozzles

    CONLEY, R. / HOFFMAN, J. / THOMPSON, H. | AIAA | 1984


    An analytical investigation of swirl in annular propulsive nozzles

    KORNBLUM, B. T. / THOMPSON, H. D. / HOFFMAN, J. D. | AIAA | 1986



    Analytical study of swirler effects in annular propulsive nozzles

    HOFFMAN, JOE D. / THOMPSON, H. DOYLE / MARCUM, DAVID L. | AIAA | 1987