AN aeroplane wing and fuselage may be treated from an analytic standpoint as two elastic beams, rigidly connected. In the present note the equations for the natural frequency, derived on the basis of Rayleigh's principle and Ritz's method, are extended to the case of free vibration of a set composed of two such beams with a number of concentrated loads elastically suspended.


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    Title :

    Vibration in Composite Beams


    Subtitle :

    A Note on Natural Frequencies of Uncoupled Flexural and Torsional Vibrations of Composite Beams


    Contributors:


    Publication date :

    1950-08-01


    Size :

    1 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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