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Mathematical Problems in Engineering
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Mathematical Problems in Engineering
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2010
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Article
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Fig 3
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Research Article
Control of Limit Cycle Oscillations of a Two-Dimensional Aeroelastic System
Figure 3
Hysteretic response of the aeroelastic system (subcritical instability). The steady-state amplitudes are plotted as a function of
U
.
(a)
Plunge motion
(b)
Pitch motion