Using simplified model of hub fuselage structure, theoretical analysis is made of response of hub and fuselage of helicopter in flight to harmonic forces transmitted by rotor blades to hub both in, and normal to, plane of rotation; expressions derived for vibration amplitudes of mass points.


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    Titel :

    Vibrations of helicopter rotor-fuselage system induced by main rotor blades in flight


    Weitere Titelangaben:

    Am Soc Mech Engrs -- Paper


    Beteiligte:
    Morduchow, M. (Autor:in) / Yuan, S.W. (Autor:in) / Reissner, H. (Autor:in)

    Kongress:

    American Society of Mechanical Engineers -- Meeting S-7 ; 1955 Vibrations



    Erscheinungsdatum :

    1955


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Vibrations of helicopter rotor-fuselage system induced by main rotor blades in flight

    Morduchow, M. / Yuan, S.W. / Reissner, H. | Engineering Index Backfile | 1955


    Helicopter fuselage vibrations induced by the rotor

    Petot, D. / Rapin, M. / France; Office national d'etudes et de recherches aerospatiales | British Library Conference Proceedings | 1996


    Helicopter Fuselage Vibrations Induced by the Rotor

    Petot, D. / Rapin, M. | British Library Conference Proceedings | 1996


    Vertical vibrations of helicopter rotor blades

    Marinescu, A. | Engineering Index Backfile | 1959


    Helicopter rotor-blades

    Engineering Index Backfile | 1955