{"title":"Reynolds number effects on the flow around a 4:1 rectangular cylinder","authors":"Hongyu Zhu , Haotian Dong , Xiaoqing Du","doi":"10.1016/j.ijmecsci.2025.110541","DOIUrl":null,"url":null,"abstract":"<div><div>Two-dimensional (2D) laminar and three-dimensional (3D) large-eddy simulations (LES) are performed to comprehensively investigate the flow dynamics and aerodynamic characteristics of uniform flow around a 4:1 rectangular cylinder at Reynolds number <em>Re</em> = 1–1.2 × 10<sup>5</sup>. Four distinct flow regimes are found: steady flow (Regime Ⅰ, <em>Re</em> < 92), unsteady laminar flow (Regime Ⅱ, 92 ≤ <em>Re</em> < 4.5 × 10<sup>2</sup>), wake transition (Regime Ⅲ, 4.5 × 10<sup>2</sup> ≤ <em>Re</em> < 7.0 × 10<sup>2</sup>), and shear layer transition (Regime Ⅳ, 7.0 × 10<sup>2</sup> ≤ <em>Re</em> ≤ 1.2 × 10<sup>5</sup>). In Regime I, for <em>Re</em> < 3 (Regime I-a), flow fully attaches to surfaces, namely 'creeping' flow; for 3 ≤ <em>Re</em> < 92 (Regime Ⅰ-b), flow separates from trailing edges, forming a steady recirculation region in the wake, namely steady separated regime. In Regime Ⅱ, for 92 ≤ <em>Re</em> < 1.2 × 10<sup>2</sup> (Regime Ⅱ-a), flow separates from trailing-edge corners and forms laminar Kármán vortices; for 1.2 × 10<sup>2</sup> ≤ <em>Re</em> < 3.0 × 10<sup>2</sup> (Regime Ⅱ-b), flow separates from leading-edge corners, reattaches to lateral surfaces with symmetrical steady separation bubbles, and separates again from trailing-edge corners; for 3.0 × 10<sup>2</sup> ≤ <em>Re</em> < 4.5 × 10<sup>2</sup> (Regime Ⅱ-c), flow changes from Kármán vortices to impinging-leading-edge-vortex (ILEV) instability, causing Strouhal number (<em>St</em>) to suddenly drop from 0.162 (<em>Re</em> = 2.75 × 10<sup>2</sup>) to 0.130 (<em>Re</em> = 3.0 × 10<sup>2</sup>). In Regime Ⅲ, wake vortices transition from laminar to turbulence with ILEV instability. In Regime Ⅳ, separated shear layers transition to turbulence, and transition position moves upstream as <em>Re</em> increases.</div></div>","PeriodicalId":56287,"journal":{"name":"International Journal of Mechanical Sciences","volume":"301 ","pages":"Article 110541"},"PeriodicalIF":7.1000,"publicationDate":"2025-06-24","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Mechanical Sciences","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0020740325006241","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0
Abstract
Two-dimensional (2D) laminar and three-dimensional (3D) large-eddy simulations (LES) are performed to comprehensively investigate the flow dynamics and aerodynamic characteristics of uniform flow around a 4:1 rectangular cylinder at Reynolds number Re = 1–1.2 × 105. Four distinct flow regimes are found: steady flow (Regime Ⅰ, Re < 92), unsteady laminar flow (Regime Ⅱ, 92 ≤ Re < 4.5 × 102), wake transition (Regime Ⅲ, 4.5 × 102 ≤ Re < 7.0 × 102), and shear layer transition (Regime Ⅳ, 7.0 × 102 ≤ Re ≤ 1.2 × 105). In Regime I, for Re < 3 (Regime I-a), flow fully attaches to surfaces, namely 'creeping' flow; for 3 ≤ Re < 92 (Regime Ⅰ-b), flow separates from trailing edges, forming a steady recirculation region in the wake, namely steady separated regime. In Regime Ⅱ, for 92 ≤ Re < 1.2 × 102 (Regime Ⅱ-a), flow separates from trailing-edge corners and forms laminar Kármán vortices; for 1.2 × 102 ≤ Re < 3.0 × 102 (Regime Ⅱ-b), flow separates from leading-edge corners, reattaches to lateral surfaces with symmetrical steady separation bubbles, and separates again from trailing-edge corners; for 3.0 × 102 ≤ Re < 4.5 × 102 (Regime Ⅱ-c), flow changes from Kármán vortices to impinging-leading-edge-vortex (ILEV) instability, causing Strouhal number (St) to suddenly drop from 0.162 (Re = 2.75 × 102) to 0.130 (Re = 3.0 × 102). In Regime Ⅲ, wake vortices transition from laminar to turbulence with ILEV instability. In Regime Ⅳ, separated shear layers transition to turbulence, and transition position moves upstream as Re increases.
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