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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    Title :

    Coupling technique of rotor-fuselage dynamic analysis


    Additional title:

    Kopplungsmethode zur dynamischen Analyse von Rotor und Rumpf


    Contributors:
    Tang, D.M. (author) / Wang, M.Q. (author)

    Published in:

    Publication date :

    1983


    Size :

    4 Seiten, 7 Bilder, 1 Tabelle, 5 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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