A jet propulsion exhaust nozzle particularly useful in multi-engine installations is described. The exhaust nozzle provides high internal/external, thrust-minus-drag, performance for transonic cruise or transonic acceleration as well as improved performance at subsonic and supersonic speeds. A two dimensional wedge/translating shroud at the nozzle exit gives the variable nozzle exit geometry needed to achieve high engine performance over a wide range of throttle power settings.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Two Dimensional Wedge/Translating Shroud Nozzle


    Beteiligte:
    D. L. Maiden (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch