2017
DOI: 10.1007/s12205-017-0239-0
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Drag Reduction on a Square Cylinder using Multiple Detached Control Cylinders

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Cited by 11 publications
(14 citation statements)
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“…It can be seen from Figure 5a-c that the shed vortices are observed only at the downstream location of the channel and the strength of shed vortices for small size of control rods (i.e., d1 = 4 is maximum as compared to d1 = 16 for g = 4). This flow mode is also observed at (g, d1) = (3, 12), (3,16), (3,20), (4,4), and (4,20). Igarashi and Suzuki [29] also investigated this flow behavior and named this mode as with reattachment and roll up flow for three circular rods.…”
Section: Rolled Up Shear Layer Reattachment (Rslr) Flow Modesupporting
confidence: 55%
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“…It can be seen from Figure 5a-c that the shed vortices are observed only at the downstream location of the channel and the strength of shed vortices for small size of control rods (i.e., d1 = 4 is maximum as compared to d1 = 16 for g = 4). This flow mode is also observed at (g, d1) = (3, 12), (3,16), (3,20), (4,4), and (4,20). Igarashi and Suzuki [29] also investigated this flow behavior and named this mode as with reattachment and roll up flow for three circular rods.…”
Section: Rolled Up Shear Layer Reattachment (Rslr) Flow Modesupporting
confidence: 55%
“…The fourth flow mode was observed at (g, d1) = (1, 12), (2,12), and (2,16). The vorticity contours of steady flow mode are shown in Figure 6a,b.…”
Section: Steady Flow (Sf) Modementioning
confidence: 93%
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