The vibration phenomena occurring during takeoff and landing of a helicopter were experimentally and theoretically investigated. The investigation covers vibrations of simplified two- and three-dimensional rotor systems. In the mathematical treatment additional degrees of fuselage freedom were taken into account. The existence of as yet unknown instability regions is pointed out with this extended theory.


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    Titel :

    A Spatial Theory for the Ground Resonance of Helicopters


    Beteiligte:
    R. Schroeder (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    181 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Ground resonance of helicopters

    Howarth, R.M. / Jones, C.H. | Engineering Index Backfile | 1953


    Ground resonance of helicopters

    Howarth, R.M. / Jones, C.H. | Engineering Index Backfile | 1953




    ROBUST APPROACH FOR GROUND RESONANCE AEROSERVOELASTIC STABILITY OF HELICOPTERS

    Quaranta, G. / Masarati, P. / Lovera, M. et al. | British Library Conference Proceedings | 2013