Print Email Facebook Twitter Note on the gust allevation factor for helicopters and autogyros Title Note on the gust allevation factor for helicopters and autogyros Author Gould, D.G. Institution National Research Council Canada, National Aeronautical Establishment, Flight Research Section Date 1966-09-30 Abstract Expressions are given for estimating the nor mal acceleration response of helicopters and autogyros to the vertical turbulence component. A gust alleviation [actor analogous to that used for fixed-wing aircra[t is derived in terms of forward velocity and the vertical damping parameter. This gust a lleviation factor compares closely with that experimentally determined for the Sycamore and Whirlwind helicopters To reference this document use: http://resolver.tudelft.nl/uuid:30076d69-7782-47ee-87a0-7254dc4b777c Publisher National Research Council Canada Access restriction Campus only Source National Research Council Aeronautical Report LR 464 Part of collection Aerospace Engineering Reports Document type report Rights (c)1966 National Research Council Canada Files PDF LR-464.pdf 3.19 MB Close viewer /islandora/object/uuid:30076d69-7782-47ee-87a0-7254dc4b777c/datastream/OBJ/view