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Mathematical Problems in Engineering
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2021
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Article
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Fig 13
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Research Article
Effect of Stiffness on Flutter of Composite Wings with High Aspect Ratio
Figure 13
Time response histories under 0.8 Ma. (a)
= 142.6 m/s, (b)
= 155.7 m/s, and (c)
= 170.8 m/s.
(a)
(b)
(c)