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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    Titel :

    Helicopter ground resonance


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Hooper, W.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Helicopter Ground Resonance

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


    Simplified Helicopter Ground Resonance Stability Boundaries

    Price, H.L. | Emerald Group Publishing | 1962



    Nonlinear Analysis of Helicopter Ground Resonance

    Kunz, D. L. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers et al. | British Library Conference Proceedings | 2000