Numerical investigation of transitions in flow states and variation in aerodynamic forces for flow around square cylinders arranged inline |
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Authors: | Waqas SARWAR ABBASI Shams UL ISLAM Lubna FAIZ Hamid RAHMAN |
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Affiliation: | 1. Mathematics Department, Air University, Islamabad 44000, Pakistan;2. Mathematics Department, COMSATS Institute of Information Technology, Islamabad 44000, Pakistan;3. Mathematics and Statistics Department, Bacha Khan University, Charsadda 44000, Pakistan |
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Abstract: | This study focuses on the transitions in flow states around two-, three- and four-inline square cylinders under the effect of Reynolds numbers at two different gap spacing values using the lattice Boltzmann method. For this purpose, Reynolds number is varied in the range 1–130 while two different values of spacing taken into account are gap spacing?=?2 and 5. Before going to actual problem, the code is tested for flow around a single square cylinder by comparing the results with experimental and numerical results of other researchers, and good agreement is found. The current numerical computations yield that for both spacing values and all combinations of cylinders there exist three different sates of flow depending on Reynolds numbers: steady state, transitional state and unsteady state. It is found that the range of Reynolds numbers for these flow states is different for both spacing values. At gap spacing?=?2 the range of Reynolds numbers for each flow state decreases by increasing the number of cylinders while at gap spacing?=?5 opposite trend is observed. The results also show that at gap spacing?=?2 the reduction in drag force is greater than the corresponding reduction at gap spacing?=?5. The maximum reduction in drag force is observed at Reynolds numbers?=?1 at both spacing values. Similarly, at both spacing values and all Reynolds numbers, the maximum reduction in drag force is observed for the case of four-inline square cylinders. |
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Keywords: | Drag reduction Flow states Gap spacing Inline cylinders Reynolds number |
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