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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    Titel :

    Study of bending-torsion aeroelastic modes for aircraft wings


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Goland, M. (Autor:in) / Luke, Y.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1949


    Format / Umfang :

    8 pages


    Anmerkungen:

    Diagrams


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Aeroelastic stability of aircraft with circulation control wings

    HAAS, DAVID / CHOPRA, INDERJIT | AIAA | 1989


    Nonlinear aeroelastic analysis of aircraft with high-aspect-ratio wings

    Patil, Mayuresh / Hodges, Dewey / Cesnik, Carlos | AIAA | 1998