Flutter modeling techniques have been successfully extended to the difficult case of the active suppression of flutter. The demonstration was conducted in a transonic dynamics tunnel using a 1/30 scale, elastic, dynamic model of a Boeing B-52 control configured vehicle. The results from the study show that with the flutter suppression system operating there is a substantial increase in the damping associated with the critical flutter mode. The results also show good correlation between the damping characteristics of the model and the aircraft.


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    Titel :

    A wind-tunnel investigation of a B-52 model flutter suppression system


    Beteiligte:
    Redd, L. T. (Autor:in) / Gilman, J., Jr. (Autor:in) / Cooley, D. E. (Autor:in) / Sevart, F. D. (Autor:in)

    Kongress:

    Structures, Structural Dynamics and Materials Conference ; 1974 ; Las Vegas, NV, US


    Erscheinungsdatum :

    01.04.1974


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Wind-Tunnel Investigation of a B-52 Model Flutter Suppression System

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