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Time-averaged topological flow patterns and their influence on vortex shedding of a square cylinder in crossflow at incidence
Authors:RF Huang  BH Lin  SC Yen
Institution:1. Department of Mechanical Engineering, National Taiwan University of Science and Technology, Taipei, Taiwan 106, Republic of China;2. Department of Mechanical and Mechatronic Engineering, National Taiwan Ocean University, Keelung, Taiwan 202, Republic of China;1. Mechanical Engineering Department, SRM University, NCR Campus, Ghaziabad, Uttar Pradesh - 201204, India;2. Mechanical & Industrial Engineering Department, Indian Institute of Technology Roorkee, Roorkee, Uttarakhand - 247667, India;3. Mechanical Engineering Department, Shri Govindram Seksaria Institute of Technology and Science, Indore, Madhya Pradesh - 452003, India;1. Department of Mechanical and Mechatronic Engineering, National Taiwan Ocean University, Keelung 202, Taiwan, ROC;2. Department of Aeronautics and Astronautics, R.O.C. Air Force Academy, Kaohsiung 820, Taiwan, ROC
Abstract:Flow characteristics around the square cylinder and their influence on the wake properties are studied. Time-averaged flow patterns on the surfaces of square cylinder in a cross-stream at incidence are experimentally probed by surface-oil flow technique and analyzed by flow topology for Reynolds numbers between 3.9×104 and 9.4×104 as the incidence angle changes from 0° to 45°. Vortex shedding characteristics are measured by a single-wire hot-wire anemometer for Reynolds numbers between 5×103 and 1.2×105. The effects of topological flow patterns on the wake properties then are revealed and discussed. Flows around the square cylinder are identified as three categories: the subcritical, supercritical, and wedge flows according to the prominently different features of the topological flow patterns. The Strouhal number of vortex shedding, turbulence in the wake, and wake width present drastically different behaviors in different characteristic flow regimes. A critical incidence angle of 15° separates the subcritical and supercritical regimes. At the critical incidence angle the wake width and shear-layer turbulence present minimum values. The minimum wake width appearing at the critical incidence angle, which leads to the maximum Strouhal number, is due to the reattachment of one of the separated boundary layer to the lateral face of the square cylinder. If the Strouhal numbers are calculated based on the wake width instead of the cross-stream projection width of cylinder, the data in the subcritical and supercritical regimes are well correlated into two groups, which would approach constants at high Reynolds numbers.
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