Supersonic transports will require jet engine thrust nozzles that are highly efficient from takeoff to supersonic cruise to minimize direct operating costs; variable-area ejectors, plug nozzles, and modifications of basic types were tested extensively at Pratt and Whitney Aircraft; performance trends for nozzles are presented with emphasis on external flow effects; new ejector which utilizes aerodynamically actuated doors to admit external air into ejector shroud is described.


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    Title :

    Thrust nozzles for supersonic transport aircraft


    Additional title:

    ASME -- Paper


    Contributors:
    Migdal, D. (author) / Horgan, J.J. (author)

    Conference:

    ASME Meeting AHGT-73 ; 1963 Ejectors



    Publication date :

    1963


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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