Theoretical analysis is presented of flutter of flat simply supported stiffened panels in supersonic flow; boundaries show that flutter speed for stiffened panels is strongly dependent on type of normal mode shape chosen; it was found that lowest stability boundary was produced for first torsional free vibration mode, whereas higher vibration modes showed no flutter; results also indicate that flutter speeds for stiffened panels are higher than those for nonstiffened panels under same conditions. (22903)


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    Titel :

    Stiffened panel flutter in supersonic flow


    Weitere Titelangaben:

    AIAA Student J


    Beteiligte:
    Vaicaitis, R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :