The development of the model 727 airplane high lift system is treated in two parts: aerodynamics, and structural and mechanical design. Part one explains the high lift requirements and traces flap design evolution from a theoretical viewpoint. It discusses trailing edge flaps, leading edge devices, flap geometry, and transition flaps, and presents results of the flight test program. Part two describes design evolution from a mechanical viewpoint. Flap system configuration and construction are detailed.


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    Titel :

    Development of the Model 727 Airplane High Lift System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    1965 International Automotive Engineering Congress and Exposition ; 1965



    Erscheinungsdatum :

    01.02.1965




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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