Aspects of design and construction of smallest of autogiro aircraft; with disk loading of under 2 psf ultralight autogiro can be almost powered parachute and be used where cost of any other aircraft would be totally prohibitive; considerations of design objectives; it is concluded that little aircraft will be pusher, with 2-bladed teetering rotor, and pre-flight rotor spinup; component design, such as rotor head, blades, fuselage, undercarriage, etc; example of autogiro, performance and improvements.


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    Title :

    Low-cost autogyro


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1963


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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