Expressions are given for estimating normal acceleration response of helicopters and autogyros to vertical turbulence component; gust alleviation factor analogous to that used for fixed-wing aircraft is derived in terms of forward velocity and vertical damping parameter; this gust alleviation factor compares closely with that experimentally determined for Sycamore and Whirlwind helicopters.


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    Titel :

    Note on gust alleviation factor for helicopters and autogyros


    Weitere Titelangaben:

    Canada. Nat Research Council -- Aeronautical Report


    Beteiligte:
    Gould, D.G. (Autor:in)


    Erscheinungsdatum :

    1966


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Gust alleviation factor

    Zbrozek, J. K. | SLUB | 1958


    Gust alleviation

    Phillips, W. H. | NTRS | 1971


    Gust response of helicopters

    Bir, Gunjit Singh | TIBKAT | 1987


    Advanced Modeling and Flight Control Design for Gust Alleviation on Ship-Based Helicopters

    Geiger, D. / Sahasrabudhe, V. / Horn, J. et al. | British Library Conference Proceedings | 2008


    Gust Alleviation Boenabminderung

    G. Bruening | NTIS | 1983