Suppression of lift fluctuations on a circular cylinder by inducing the symmetric vortex shedding mode |
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| Institution: | 1. Department of Mechanical Engineering, National Taiwan University of Science and Technology, 43 Keelung Road, Section 4, Taipei, Taiwan 10672, Republic of China;2. Graduate Institute of Applied Science and Technology, National Taiwan University of Science and Technology, Taipei, Taiwan 10672, Republic of China;1. Department of Mechanical Engineering, National Institute of Technology Agartala, Tripura 799 055, India;2. Department of Aerospace Engineering, Indian Institute of Technology Kanpur, UP 208 016, India |
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| Abstract: | The flow around a stationary circular cylinder modified by two synthetic jets positioned at the mean separation points is numerically studied. The Reynolds number based on the free-stream velocity and the circular cylinder diameter is Re=500. The focus is to present a novel way to suppress the lift fluctuations by changing the vortex shedding mode, and thus particular attention is paid to the interactions between the synthetic jets and wake shear layers and the resulting vortex dynamics. The overall influences of both momentum coefficient and excitation frequency are discussed. In some simulated cases, the vortex lock-on phenomenon is discovered, which causes the typical Kàrmàn type vortex shedding to be converted into the symmetric shedding modes, leading to the complete suppression of lift fluctuations. In other cases, the asymmetric shedding mode still dominates the wake evolution. Detailed vortical evolution for each typical wake pattern is analyzed to reveal the control mechanism. Additionally, the control effectiveness is evaluated, indicating that the present control strategy contributes an effective way to suppress the lift fluctuations and reduce the mean drag. |
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| Keywords: | Flow control Wake pattern Symmetric mode Lift suppression Drag reduction |
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