Rigid body studies conducted by Battelle and NASA-Langley have indicated that free floating pivoting wings can significantly reduce turbulence induced vertical accelerations. However, NASA-Langley has shown that a flexible pivoting wing can have an unacceptably low flutter speed. Presented in this document are the results of an analytical follow-on study conducted to determine the feasibility of increasing the flutter speed with an active or passive flutter stability augmentation system (SAS) while retaining significant ride smoothing capability. (Author)


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    Titel :

    Pivoting Wing Ride Smoothing/Flutter SAS Analysis


    Beteiligte:
    W. J. Wattman (Autor:in) / J. L. Townsend (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    71 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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