Velocity-component aerodynamic-strip theory is used with quasi-steady and unsteady Theodorsen-function representations; exact solutions of differential equation are obtained, thereby eliminating problems of modal convergence; effects of structural damping and below-flutter response are also examined; below certain critical values of mass-density ratio, flutter does not occur; at low values of mass-density ratio increasing sweep-back of given wing lowers flutter speed significantly until critical angle is reached, beyond which flutter speed rises sharply to infinity.


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    Titel :

    Pure bending flutter of swept wing in high-density, low-speed flow


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Dugundji, J. (Autor:in) / Ghareeb, N. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 6 ; p 1126-1133


    Erscheinungsdatum :

    1965


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Bending-torsional flutter of swept wing in high-density, low-speed flow

    Prasad, S.N. / Nemat-Nasser, S. / Herrmann, G. | Engineering Index Backfile | 1967



    Bending-torsional flutter of a swept wing in a high-density, low-speed flow.

    Herrmann, G. / Nemat-Nasser, S. / Prasad, S. N. | NTRS | 1967