2015
DOI: 10.1016/j.engstruct.2015.05.017
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Numerical study of a twin box bridge deck with increasing gap ratio by using RANS and LES approaches

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Cited by 46 publications
(19 citation statements)
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“…1(a) and (b), a series of 1:80 simplified section models of twin-box girders without consideration of the deck secondary structures were performed in the TJ-1 Wind Tunnel of Tongji University to accommodate the size of sectional models and testing section. Since the SWR plays an important role in the aerodynamic performance of twin-box girder bridges [4,5], spring-supported rigid sectional models with five representative cases of SWR (i.e. D/Bs= 0.2, 0.4, 0.6, 0.8, and 1.0) were used in the testing to assess the control effectiveness of VCS on the flutter instability in twin-box girders bridges.…”
Section: Experimental Set-upmentioning
confidence: 99%
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“…1(a) and (b), a series of 1:80 simplified section models of twin-box girders without consideration of the deck secondary structures were performed in the TJ-1 Wind Tunnel of Tongji University to accommodate the size of sectional models and testing section. Since the SWR plays an important role in the aerodynamic performance of twin-box girder bridges [4,5], spring-supported rigid sectional models with five representative cases of SWR (i.e. D/Bs= 0.2, 0.4, 0.6, 0.8, and 1.0) were used in the testing to assess the control effectiveness of VCS on the flutter instability in twin-box girders bridges.…”
Section: Experimental Set-upmentioning
confidence: 99%
“…To determine the flow structures for twin-box girders with VCS, the Smagorinsky subgrid-scale models for fluid-structural coupling and the free oscillation method [5] were used in this study. Based on a finite volume method (FVM), the unstructured grid system incorporating large eddy simulations (LES) modeling was used to discretize the governing Navier-Stokes equations [28].…”
Section: Numerical Modelmentioning
confidence: 99%
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“…Reynolds average numerical simulations are performed using the k–ω shear stress transport (SST) model. This model is known to provide more accurate results, if compared to standard k–ω and k–ε models, in external aerodynamic cases which involve boundary layer separation (Miranda et al, 2015). The dimensionless time-step is set equal to 10 −3 .…”
Section: Aerodynamic Characteristics Of a Plate With Central Stabilizermentioning
confidence: 99%
“…This bare deck design was chosen due to the availability of experimental data for validation studies. Several CFD studies of flow characteristics around the sharp-edged twin-boxes, particularly with asymmetric geometry as in the present case, have been carried out [22][23][24]. These studies have mainly dealt with the overall flow conditions and their variations with the relative gap size, Reynolds number and turbulence models used in the simulations.…”
Section: Introductionmentioning
confidence: 99%