In this paper is introduced a method of dynamic analysis of the helicopter rotor coupled with fuselage in the rotating plane. The method has been used to determine the inplane rotor-fuselage dynamic properties of a light helicopter with fiberglass-reinforced plastics rotor blades. This paper makes particular reference to the effect of anisotropic dynamic stiffness of the rotor shaft end of fuselage on the natural dynamic characteristics.


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    Titel :

    Coupling technique of rotor-fuselage dynamic analysis


    Weitere Titelangaben:

    Kopplungsmethode zur dynamischen Analyse von Rotor und Rumpf


    Beteiligte:
    Tang, D.M. (Autor:in) / Wang, M.Q. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1983


    Format / Umfang :

    4 Seiten, 7 Bilder, 1 Tabelle, 5 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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