A jet propulsion exhaust nozzle is reported for multi-engine installations which produces 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 provides 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 :

    1978-05-09


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English