Advantages of rotating wing aircraft over fixed wing type; forces on blade due to air flow and autorotation estimated and required strength of blade calculated; formula given; investigation of bending moment on rotor blade when not rotating; theorems relating to autogyrating blade. (Aircraft Engr) (See also - n 1658 Oct 3 1940 p 275-7)


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    Title :

    Case for single-bladed rotor


    Additional title:

    Flight


    Contributors:

    Published in:

    Flight ; 38 , n 1663


    Publication date :

    1940


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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