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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Analysis and Testing of Stability Augmentation Systems


    Contributors:
    F. D. Sevart (author) / S. M. Patel (author) / W. J. Wattman (author)

    Publication date :

    1972


    Size :

    125 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    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