THE aim of this paper is to calculate the natural frequencies and to consider the influence of the damping parameter on a wing's natural flexural and torsional vibration. The author took into account only the elastic hysteresis of the material because the structural damping, depending on the type of the aeroplane, cannot be taken into account in a general consideration.


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    Titel :

    A Note on Natural Frequencies


    Untertitel :

    Natural Frequencies of Uncoupled Flexural and Torsional Oscillations with Damping of a Cantilever Wing


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.02.1949


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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