Method based on consideration of perfectly flexible helicopter rotor blades; exact solutions of fairly simple character presented for blade of uniform section and blade having uniformly decreasing sectional area down to zero at tip; solutions bring out various important points, in particular, effect of blade root conditions, especially position of flapping hinge.


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    Title :

    Natural vibration frequencies of flexible rotor blades


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1958


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Natural Vibration Frequencies of Flexible Rotor Blades

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