期刊
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS
卷 172, 期 -, 页码 298-316出版社
ELSEVIER SCIENCE BV
DOI: 10.1016/j.jweia.2017.11.016
关键词
LES; Reynolds number effects; Flow characteristics; Twin box girder; Turbulence transition
资金
- NSFC [51503138, 51161120359]
- China Postdoctoral Science Foundation [2015M580266]
- Heilongjiang Postdoctoral Fund [LBH-Z15087]
- Fundamental Research Funds for the Central Universities [HIT. NSRIF. 2017064]
A numerical investigation of Reynolds number sensitivity on flow past a twin-box girder was performed using large eddy simulation (LES) with Reynolds numbers of 1e2 <= Re <<= number sensitivity according to the flow region and the flow state. At the leading edge, the flow experiences laminar separation-laminar reattachment state (1.5e3 < Re < 6e3), laminar separation-turbulence reattachment state (6e3 <= Re <= 8e4), and turbulence separation-turbulence reattachment flow state (Re > 8e4). Around the gap, four models exist depending on Reynolds number: laminar closed cavity flow (Re < 1.6e3), laminar open cavity flow (1.6e3 <= Re <= 5e3), wake model (5e3 <= Re <= 9e3), and turbulent open cavity flow (Re > 8e3). In the tail of the box girder, a regular Karman vortex is first generated, and then the lower shear layer transits to turbulence, resulting in the generation of separation bubbles at the lower and upper trailing edges. However, due to the upper trailing edge being blunter than lower trailing edge, the Reynolds number sensitive range of upper trailing edge (1e2-1e7) is much wider than lower trailing edge (1e2-2e4).
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