Analyses and flight tests of the B-1 structural mode control system (SMCS) are presented. Improvements in the total dynamic response of a flexible aircraft and the benefits to ride qualities, handling qualities, crew efficiency, and reduced dynamic loads on the primary structures, were investigated. The effectiveness and the performance of the SMCS, which uses small aerodynamic surfaces at the vehicle nose to provide damping to the structural modes, were evaluated.


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    Titel :

    Analyses and Tests of the B-1 Aircraft Structural Mode Control System


    Beteiligte:
    J. H. Wykes (Autor:in) / T. R. Byar (Autor:in) / C. J. Macmiller (Autor:in) / D. C. Greek (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    268 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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