Several examples are presented in which flutter involving interaction between flight mechanics modes and elastic wind bending occurs for a forward swept wing flight vehicle. These results show the basic mechanism by which the instability occurs and form the basis for attempts to actively control such a vehicle.


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    Titel :

    Interactive aircraft flight control and aeroelastic stabilization


    Beteiligte:
    Weisshaar, T. A. (Autor:in) / Schmidt, D. K. (Autor:in)

    Erscheinungsdatum :

    1981-10-31


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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