Of parameters that may be adjusted to give helicopter freedom from ground resonance, that which is ignored most frequently is ratio of effective rotor mass to effective fuselage mass; if it is considered early in design of fuselage, ground resonance problem can be greatly reduced or eliminated by consideration of this parameter alone; investigation of influence of dynamic properties on rotor to fuselage effective mass ratio and its effect on stability boundaries; results obtained.


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    Titel :

    Effect of fuselage dynamics on helicopter ground resonance


    Weitere Titelangaben:

    Aircraft Eng


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

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Effect of Fuselage Dynamics on Helicopter Ground Resonance

    Hooper, W.E. | Emerald Group Publishing | 1962



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