Testing and evaluation of stability augmentation systems for aircraft flight control were conducted. The flutter suppression system analysis of a scale supersonic transport wing model is described. Mechanization of the flutter suppression system is reported. The ride control synthesis for the B-52 aeroelastic model is discussed. Model analyses were conducted using equations of motion generated from generalized mass and stiffness data. (Author)


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    Titel :

    Analysis and Testing of Stability Augmentation Systems


    Beteiligte:
    F. D. Sevart (Autor:in) / S. M. Patel (Autor:in) / W. J. Wattman (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    125 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Analysis and testing of stability augmentation systems

    Sevart, F. D. / Patel, S. M. / Wattman, W. J. | NTRS | 1972




    Design GEM stability augmentation systems

    Dukes, T.A. / Hargraves, C.R. | Engineering Index Backfile | 1963