Calculations and results given serve to show how methods referred to in previous paper ("General Approach to Flutter Problem"), are applied to particular problem in flutter; calculations described for cantilever wing which was flutter tested at NACA Laboratories and test results compared with calculated results.


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    Title :

    Use of generalized coordinates in flutter analysis


    Additional title:

    Soc Automotive Engrs -- Preprint


    Contributors:

    Conference:

    Society of Automotive Engineers -- Meeting ; 1943 Flutter



    Publication date :

    1943


    Size :

    34 pages


    Remarks:

    22 Supp sheets, Bibliography


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Use of Generalized Coordinates in FLUTTER ANALYSIS

    LORING, SAMUEL J. | SAE Technical Papers | 1944





    Flutter and Divergence Analysis Using the Generalized Aeroelastic Analysis Method

    Edwards, J. / Wieseman, C. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003