With objective of formulating realistic computing program to analyze panel flutter to aerospace vehicles, plausible simplifying assumptions are examined in light of experimental results; it is shown that in certain areas very simple analysis yields respectable results, whereas in other areas great elaboration is necessary to obtain accurate prediction; examples show that boundary layer greatly stabilizes flat plates in transonic or low supersonic flow and circular cylindrical shells at higher Mach numbers; recent contributions to panel flutter research at California Inst of Technology are summarized.


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    Title :

    Some recent contribution to panel flutter research


    Additional title:

    AIAA J


    Contributors:
    Fung, Y.C. (author)

    Published in:

    AIAA Journal ; 1 , n 4


    Publication date :

    1963


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    Contribution to the Study of ''Panel Flutter''

    R. Barboni / P. Santini | NTIS | 1966


    Research on panel flutter

    Kobett, D. R. | TIBKAT | 1964


    Research on Panel Flutter

    Kobett, D. R. / Zeydel, E. F. E. | NTRS | 1963