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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2017
/
Article
/
Fig 6
/
Research Article
A Highly Accurate Approach for Aeroelastic System with Hysteresis Nonlinearity
Figure 6
Time histories of the aeroelastic system at
U
/
U
0
ā=ā0.9 for (a) pitch and (b) plunge directions, respectively.
(a)
(b)