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.


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    Title :

    Two Dimensional Wedge/Translating Shroud Nozzle


    Contributors:

    Publication date :

    1976


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English