The aerodynamic force on an element dx1 of the rotor blade produces a moment about any point, and the component of this moment along the flapping hinge determines the flapping motion of the blade. The air force on an element being i4 dX4‘+Jt d/Y4’+k1 dZ,‘, the moment dG’, say, about the hinge F is given by


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    Title :

    Rotor Dynamics and Helicopter Stability


    Subtitle :

    Development of a Unified Mathematical Theory of the Steady and Disturbed Motion of a Helicopter with Particular Emphasis on the Dynamical Aspects of the Problem


    Contributors:
    Price, H.L. (author)

    Published in:

    Publication date :

    1963-07-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1965


    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1963


    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1964


    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1964


    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1963