Flutter of panels mounted on wedges in hypersonic flow of perfect gas is analyzed in linear formulation using S.C.McIntosh's theory; it is shown that acoustic waves generated by oscillating panels and reflected by bow shock can be neglected for virtually all practical purposes, and flutter of panel is independent of its fore-aft position on wedge; this demonstrates validity of engineering analysis in which flow parameters behind bow wave are computed using oblique shock relations and piston theory applied to panel that is parallel to this flow.


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    Titel :

    Panel flutter in hypersonic flow


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Bailie, J.A. (Autor:in) / McFeely, J.E. (Autor:in)

    Erschienen in:

    AIAA Journal ; 6 , n 2


    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    PANEL FLUTTER IN HYPERSONIC FLOW

    BAILIE, J. / MCFEELY, J. | AIAA | 1967


    Panel flutter in hypersonic flow.

    BAILIE, J. A. / MCFEELY, J. E. | AIAA | 1968


    Hypersonic panel flutter studies on curved panels

    Nydick, Ira / Friedmann, Peretz / Zhong, Xaolin | AIAA | 1995


    Hypersonic Panel Flutter Studies on Curved Panels

    Nydick, I. / Friedmann, P. / Zhong, X. et al. | British Library Conference Proceedings | 1995


    Impact of Flow and Structural Nonlinearities on Hypersonic Panel Flutter Predictions

    Schoneman, Joseph / Ostoich, Christopher / Jarman, Lucas et al. | AIAA | 2018