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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    Titel :

    Use of generalized coordinates in flutter analysis


    Weitere Titelangaben:

    Soc Automotive Engrs -- Preprint


    Beteiligte:
    Loring, S.J. (Autor:in)

    Kongress:

    Society of Automotive Engineers -- Meeting ; 1943 Flutter



    Erscheinungsdatum :

    1943


    Format / Umfang :

    34 pages


    Anmerkungen:

    22 Supp sheets, Bibliography


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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