Flow-induced vibration of an elastically mounted airfoil under the influence of the wake of a circular cylinder
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d="p0005">A Virtual Mass Spring Mechanism was used to investigate the response of a NACA 0012.

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d="p0010">The locations with higher power density were determined in the wake of the cylinder.

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d="p0015">The staggered arrangements of cylinder-airfoil show higher FIV efficiency.

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d="p0020">Physics of fluid is considered in the wake of the cylinder.

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