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This paper presents a systematic study on active flutter suppression of a high aspect-ratio wing with multiple control surfaces distributed throughout the span.
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With control using redundant multiple control surface arrangement and large-deflection drag rudders, a combat flying wing has a higher probability for control surface failures.
Various flow control methods were discussed: multiple vortices, control surfaces, blowing and suction, low-frequency and high-frequency excitation, feedback control, passive control with wing flexibility, and plasma actuators.
This scheme can handle requirements of state limiting as well as multiple redundant control surface saturation.
Blended wing body aircraft typically have multiple redundant flight control surfaces at the trailing edge with only a limited moment arm with respect to the center of gravity.
The potential of using multiple leading and trailing edge control surfaces and aeroelastic effects for efficient roll manoeuvring is investigated.
In this paper, the effects of structural nonlinearity due to free-play in both leading-edge and trailing-edge outboard control surfaces on the linear flutter control system are analyzed for an aeroelastic model of three-dimensional multiple-actuated-wing.
Control surfaces modeling and design.
So multiple control efforts may be necessary.
Multiple control points are introduced.
Internal components and control surfaces of the V-2 missile.
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