Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle designed for flight Mach numbers to 3.0


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    Title :

    Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0


    Contributors:

    Publication date :

    1961-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English