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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    Title :

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


    Additional title:

    AIAA J


    Contributors:
    Lock, M.H. (author) / Farkas, E.F. (author)

    Published in:

    AIAA Journal ; 3 , n 9


    Publication date :

    1965


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :