The basic objective of this work is to provide a direct and simple means for calculating classical flutter. The analysis makes no use of free vibration modes, although the method is readily adaptable to a modal type approach. Only subsonic aerodynamics are considered; however, the method applies to any speed regime. The problems of following modes and modal coupling are completely avoided. The simplicity and accuracy of the direct solution is stressed. The analysis is applicable to both straight and swept wings although only straight wings, uniform as well as nonuniform, are presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    A direct method for calculating flutter speeds


    Beteiligte:
    Beres, D. P. (Autor:in)

    Kongress:

    Aerospace Sciences Meeting ; 1974 ; Washington, DC


    Erscheinungsdatum :

    01.01.1974


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Flutter at very high speeds

    Runyan, Harry L. / Morgan, Homer G. | TIBKAT | 1961


    Flutter at very high speeds

    Runyan, Harry L / Morgan, Homer G | NTRS | 1957


    Flutter model testing at transonic speeds

    Targoff, W.P. / White, Jr., R.P. | Engineering Index Backfile | 1957