2026· Mechanics & Industry· Vol 27, pp. 37· 0 citations· 25 references
Abstract
This study focuses on the irregular staggered bluff body structure formed by the main tower and its hoisted steel transverse girders of large-span bridges. Existing research is difficult to adapt to the dynamic spacing of hoisting, and cannot provide theoretical support for wind-induced safety control during construction. Taking the Chishi Bridge as the object, the SST
k-ω
turbulence model is used for numerical simulation. The vertical spacing ratio (
Q*
), horizontal spacing ratio (
S*
), wind speed (“v”), and wind angle of attack (α) are adopted as the core variables. The aerodynamic interference intensity is quantified by the three-component force coefficient interference factor, and the influence of each parameter on the aerodynamic flow around the suspended steel crossbeam is analyzed. The results show that under symmetric inflow, the base of lift and torque coefficients are small, and aerodynamic interference mainly manifests as changes in drag coefficient. When the spacing changes, the vortex coupling, blockage effect, and suction effect dominate the change in resistance. As the wind speed increases, all interference factors increase. The increase in wind attack angle has a relatively small impact on drag interference. However, it will cause a linear increase in lift and torque interference factors through the asymmetric flow field double amplification effect of staggered structures. The results reveal the flow field evolution mechanism of the staggered blunt body flow, providing a theoretical basis for wind-induced safety control during the steel crossbeam hoisting stage of the bridge tower.
Under crosswind conditions, multiple flow separations occur in the leeward side (LWS) region of the trains, leading to the formation of large-scale vortical structures that reduce surface pressure and generate significant lateral aerodynamic loads. Disrupting these large-scale vortices and increasing the LWS pressure t...
Ao Xu, Fengyi Huang, Xiao-Hui Xiong et al.· The Physics of Fluids· 0 citations
This article analyzes the aerodynamic characteristics of the NACA2412 and NACA23012 airfoils under low angles of attack. Computational fluid dynamics (CFD) numerical simulation is used to design geometric models and perform mesh generation, while the data were analyzed using a finite element method to calculate lift...
Ji-Xiang Huang· MATEC Web of Conferences· 0 citations
Formula SAE (Society of Automotive Engineers) vehicles usually operate under low-speed cornering conditions, where the front wing is required to generate stable downforce to improve tire grip and handling performance.This paper investigates the effect of flap deflection angle on the downforce of a simplified two-elemen...
Da Chen· Applied and Computational En...· 0 citations
This study examines the hovering and forward-flight stability of a heavy-lift coaxial unmanned helicopter with a suspended payload. A six-degree-of-freedom dynamics model is developed, coupling the rotor, fuselage, and a rigid-body sling via a universal joint, while neglecting rotor–payload aerodynamic interference for...
Archimedes Spiral Wind Turbines (ASWTs) are suitable for small-scale urban wind applications, but changing the blade angle can also change the rotor dimensions under different geometric constraints. This study examines these coupled effects by comparing five ASWT configurations with blade angles of 30°, 45°, and 60° un...
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As high-speed railway technology advances rapidly, aerodynamic safety under crosswind conditions has become a critical engineering concern. This study investigates the aerodynamic characteristics of the CR450 high-speed train under various track topographies—including viaducts, embankments, and cuttings—equipped with...
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