Examination of way in which ground resonance properties of helicopter depend on fuselage damping, blade damping, drag hinge offset, inter-blade spring stiffness, blade mass and angular velocity of rotor as specified by given parameters; method of exact stability criteria for helicopters on isotropic supports; geometry drawing stability boundaries as remaining parameters vary is studied; case of rotor having inter-blade friction damping as against viscous damping. (See also - n 376 June 1960 p 156-60)


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    Titel :

    Avoidance of ground resonance


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Price, H.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    The Avoidance of Ground Resonance

    Price, H.L. | Emerald Group Publishing | 1960


    The Avoidance of Ground Resonance

    Price, H.L. | Emerald Group Publishing | 1960


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