Performance characteristics of auxiliary inlet ejector nozzle configurations for takeoff, transonic acceleration, and supersonic flight conditions with pressure and temperature profiles


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    Title :

    Static performance of an auxiliary inlet ejector nozzle using an afterburning turbojet gas generator


    Contributors:

    Publication date :

    1970-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English