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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    Title :

    Flutter research on skin panels


    Additional title:

    NASA -- Tech Note


    Contributors:
    Kordes, E.E. (author) / Tuovila, W.J. (author) / Guy, L.D. (author)


    Publication date :

    1960


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Flutter research on skin panels

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    Flutter research on skin panels

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


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    Flutter design of stiffened-skin panels for hypersonic aircraft

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