Flutter boundaries obtained from experiments are compared with various theoretical predictions; modal analysis of Donnell's equations is used in conjunction with piston theory and potential solution of R.W.Leonard and J.M.Hedgepeth; it was found that pressurized cylindrical shells fluttered at lower level of freestream energy than predicted by either theory; of two results, that using piston theory appears to correspond more closely to experiment.


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    Titel :

    Comparing theory and experiment for supersonic flutter of circular cylindrical shells


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Olson, M.D. (Autor:in) / Fung, Y.C. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 10


    Erscheinungsdatum :

    1967


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :