Supersonic flutter analysis of infinite span plate, separated into array of rectangular panels, is presented; region between Mach 1 and 2 1/2 is of interest, and linearized three-dimensional aerodynamic theory is applied; elastic behavior of configuration is described by small deflection theory; partially clamped edge condition is obtained by introducing torsional restraint proportional to first derivative of transverse deflection along normal to edge; numerical results are given in terms of characteristic panel flutter parameters.


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    Titel :

    Flutter of flat plates with partially clamped edges in low supersonic region


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Zeydel, E.F.E. (Autor:in) / Kobett, D.R. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 1


    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :