Paper describes methods and results of coordinated experimental and theoretical investigation of flutter of flat, rectangular, isotropic panels; theoretical calculations are based upon classical, small, deflection-plate theory and three-dimensional, unsteady, aerodynamic theory, as well as simpler theories; effect of dynamics of air in sealed cavity beneath panel is accounted for; experimental program is described, including presentation of pertinent data and comparison with theory.


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    Titel :

    Theoretical and experimental panel flutter studies in mach number range 1.0 to 5.0


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Dowell, E.H. (Autor:in) / Voss, H.M. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 12


    Erscheinungsdatum :

    1965


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Some experimental studies of panel flutter at Mach number 1.3

    Sylvester, Maurice A. / Baker, John E. | TIBKAT | 1957


    Some experimental studies of panel flutter at Mach number 1.3

    Sylvester, Maurice A / Baker, John E | NTRS | 1952


    Experimental and theoretical studies of panel flutter at Mach numbers 1.2 to 3.0

    Sylvester, Maurice A / Nelson, Herbert C / Cunningham, Herbert J | NTRS | 1955