Attention drawn to powerful influence of Coriolis forces and flapping pin offset on stability; for conventional rotor of small offset, damping in pitch and flight stability are greatly reduced by absence of drag hinges.


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    Title :

    Helicopter stability in hovering flight


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Payne, P.R. (author)

    Published in:

    Publication date :

    1955


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :