Equations of motion developed by R.P.COLEMAN evaluated for particular configuration and large number of different combinations of rotor and fuselage damping; results, displayed graphically, reveal dependence of unstable range on rotor and fuselage damping; ground resonance stated to be stability problem, closely analogous to problem of flutter.


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    Title :

    Helicopter ground resonance


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1959


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Helicopter Ground Resonance

    Hooper, W.E. | Emerald Group Publishing | 1959



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