Two-dimensional flutter of two-bay clamped-edge and simply supported panels at supersonic Mach numbers is studied to determine influence of structural and aerodynamic coupling; it is found that effect of structural coupling between panel bays is unimportant both for single-degree-of-freedom flutter modes that are critical at lower supersonic Mach numbers and for critical coupled flutter modes that develop at higher supersonic Mach numbers; effect of aerodynamic coupling is of importance for single-degree-of-freedom flutter modes only; severity of effect is highly dependent on panel boundary conditions.


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    Titel :

    Flutter of two-bay flat panels of infinite span at supersonic Mach numbers


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Lock, M.H. (Autor:in) / Farkas, E.F. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 9


    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :