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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    Titel :

    Thrust nozzles for supersonic transport aircraft


    Weitere Titelangaben:

    ASME -- Paper


    Beteiligte:
    Migdal, D. (Autor:in) / Horgan, J.J. (Autor:in)

    Kongress:

    ASME Meeting AHGT-73 ; 1963 Ejectors



    Erscheinungsdatum :

    1963


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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