Aerodynamic problems of achieving efficient turbojet exit nozzle installations for operation over wide speed range; particular attention devoted to influence of jet stream interaction on both nozzle thrust and afterbody drag; for this purpose, use is made of shock boundary layer interaction concepts.


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    Title :

    Some aerodynamic considerations of nozzle-afterbody combinations


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1956


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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