| 摘要 |
There is provided a rotary-wing aircraft (12,200) comprising:
a main rotor (14);
a tail boom (22,60), wherein at least a portion of the tail boom (22,60) is located in an area of downwash (26) from the main rotor (14);
a yaw-control member (37,68) movably coupled to the tail boom (22,60) and
a linear nozzle (33,62) mounted on the tail boom (22,60) and having an opening extending along the tail boom (22,60), the linear nozzle (35,62) being adapted to discharge a sheet of fluid (43) in a direction substantially tangential to an outer surface (22a) of the tail boom (22,60).
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