Results for unstiffened rectangular panels and panels stiffened by corrugated backing are presented and flutter boundaries established for all types of panels when considered on basis of equivalent isotropic plates; effects of Mach number, differential pressure, and aerodynamic heating on panel flutter; flutter analysis of orthotropic panels.


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    Titel :

    Flutter research on skin panels


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Kordes, E.E. (Autor:in) / Tuovila, W.J. (Autor:in) / Guy, L.D. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Flutter research on skin panels

    Kordes, Eldon E. / Tuovila, Weimer J. / Guy, Lawrence D. | TIBKAT | 1960


    Flutter research on skin panels

    Kordes, E. E. / Tuovila, W. J. / Guy, L. D. | NTRS | 1960


    Transonic Flutter of Skin Panels Pinned at the Center

    Currao, Gaetano M. D. / He, Hsu-Chang | AIAA | 2024

    Freier Zugriff

    Flutter design of stiffened-skin panels for hypersonic aircraft

    Anderson, M. S. / Bohon, H. L. / Heard, W. L., Jr. | NTRS | 1969


    Flutter design of stiffened-skin panels for hypersonic aircraft

    Bohon, H. L. / Anderson, M. S. / Heard, W. L., Jr. | NTRS | 1967