Theory presented of ejector nozzle in which secondary shroud is cylindrical, which is based on continuity, momentum and maximizing of secondary flow; good agreement with experiment obtained.


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    Title :

    Theory of cylindrical ejector supersonic propelling nozzle


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Pearson, H. (author) / Holliday, J.B. (author) / Smith, S.F. (author)

    Published in:

    Publication date :

    1958


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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