Sample calculations presented for series of wings subject to bending vs torsion flutter, showing how natural mode dampings and frequencies change as flutter speed is approached; comparison between normal mode characteristics and system response due to forced excitation.


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    Title :

    Study of bending-torsion aeroelastic modes for aircraft wings


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Goland, M. (author) / Luke, Y.L. (author)


    Publication date :

    1949


    Size :

    8 pages


    Remarks:

    Diagrams


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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