Influence of the presence of a flat plate on the flow behavior around a smooth and rigid circular cylinder
DOI:
https://doi.org/10.5216/reec.v21i1.79811Keywords:
Vortex shedding, Circular cylinder, Boundary layer, Drag coefficient, Lift coefficientAbstract
ABSTRACT: In some engineering applications, circular cylinders near flat boundaries are often subjected to flows normal to their axes. Physical simulations with this type of arrangement are typically conducted with cylinders mounted close to flat plates inside wind or water tunnels. In the present study, vortex shedding and aerodynamic coefficients of a smooth, rigid circular cylinder immersed in a flow near a flat plate were experimentally investigated. The experiments were performed with two distinct incident flows, with a Reynolds number, based on the cylinder diameter (D), of 3.1 × 10⁴. The boundary layer thicknesses (δ) of these flows were 1D and 1.4D. The results showed that both the drag coefficient (CD) and the lift coefficient (CL) were strongly influenced by the ratio of the distance between the cylinder and the plate (G/D), and that δ affected these coefficients unevenly. Analysis of the power spectra of hot-wire signals and CL signals indicated that the alternate vortex shedding was suppressed when G/D fell below a certain critical value – (G/D)cr. The (G/D)cr was 0.4 for δ = 1D and 0.3 for δ = 1.4D. Through the power spectral analysis, it was also possible to confirm results from previous studies that the Strouhal number in the intermediate range of the subcritical regime is practically insensitive to the presence of the plate when G/D > (G/D)cr.
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