Aerodynamic principles involved in design and operation of this craft are discussed; all Autogiros so far have standard airplane fuselage, landing gear and tail unit; rotating system of supporting surfaces in place of wings; ailerons are separate organs carried on each side of fuselage; blades in addition to rotating, move up and down; speed of vane system constant; auxiliary drive being developed will allow spinning up of rotating wings directly by main engine.


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    Titel :

    The Cierva autogiro


    Weitere Titelangaben:

    Aviation


    Beteiligte:
    Sayers, W.H. (Autor:in)

    Erschienen in:

    Aviation ; 25 , n 18


    Erscheinungsdatum :

    1928


    Anmerkungen:

    8 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Cierva Autogiro Co., Ltd.

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