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.
Note on gust alleviation factor for helicopters and autogyros
Canada. Nat Research Council -- Aeronautical Report
1966
26 pages
Report
Englisch
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