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Shock and Vibration
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2021
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Article
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Fig 6
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Research Article
Kinematic Optimization of a Flexible Wing Undergoing Flapping and Pitching
Figure 6
The lift coefficient and thrust coefficient in a complete cycle: (a) 60, 90, and 120 bound vortices; (b) 15, 20, and 25 chord-length wakes.
(a)
(b)