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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    Title :

    Note on gust alleviation factor for helicopters and autogyros


    Additional title:

    Canada. Nat Research Council -- Aeronautical Report


    Contributors:
    Gould, D.G. (author)


    Publication date :

    1966


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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