Theoretical approach with object of determining natural frequencies and hub characteristics of single rotor helicopter in free ground vibration for use in analysis of self excited mechanical oscillations of hinged rotor blades; method is intended to obviate experimental determination of these parameters.


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    Title :

    Helicopter in free ground vibration


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1952


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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