General characteristics of panel flutter are examined theoretically; linear plate theory and two-dimensional first-order aerodynamics are used; paper attempts to clarify important role of damping, relationship between traveling and standing wave theories of panel flutter, and effects of edge conditions; solution procedures and general mathematical behavior may be of interest in other stability problems characterized by appearance of complex eigenvalues.


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    Title :

    Theoretical considerations of panel flutter at high supersonic Mach numbers


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 4 , n 7


    Publication date :

    1966


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :