Drag and wake regime control of flow past tandem circular cylinders using hinged splitter plate: A numerical investigation
ORAL
Abstract
In the present numerical study, the drag and wake regime control of two-dimensional tandem identical circular cylinders (TCC) with a hinged splitter plate (HSP) at a Reynolds number of Re = 100 is investigated using the inhouse developed flexible forcing immersed boundary scheme-based one-step simplified lattice Boltzmann method. The gap G between the centres of the cylinders is set at G = 5.0D, where D is the diameter of the cylinder. The rigid splitter plate is hinged at the rear base point of the upstream cylinder, and it undergoes a sinusoidal pitching motion for the pitching amplitudes (θm) of 15º. In addition, the Strouhal number (Stf) and the splitter plate length (Lf) are varied between 0.1 – 0.4 and 0.0D – 1.0D, respectively. It is observed that the total drag of TCC with HSP configuration is always less compared to the stationary splitter plate of identical size. Moreover, the total drag of TCC-HSP arrangement decreases for increasing Stf at all Lf except when Lf = 1.0D, and a maximum of 35% drag reduction is achieved at Stf = 0.40 and Lf = 0.75D. However, beyond Stf ≥ 0.20, the total drag of TCC increases for Lf = 1.0D. The relationship between drag and the near wake flow structure will be thoroughly discussed in the presentation for varied Stf and Lf.
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Presenters
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Prabir Sikdar
Indian Institute of Technology Kharagpur.
Authors
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Prabir Sikdar
Indian Institute of Technology Kharagpur.
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Sunil Manohar Dash
Department of Aerospace Engineering, Indian Institute of Technology Kharagpur, West Bengal, India – 721302
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Kalyan Prasad Sinhamahapatra
Department of Aerospace Engineering, Indian Institute of Technology Kharagpur, West Bengal, India - 721302