阻力
转向架
空气动力阻力
空气动力学
还原(数学)
物理
湍流
翼
海洋工程
涡流
分离涡模拟
机械
航空航天工程
升力诱导阻力
雷诺平均Navier-Stokes方程
工程类
机械工程
几何学
数学
作者
Chen Jiang,Y Li,Jin-lan Long,Xin Tang,Guangjun Gao,Franklin C. Eze
出处
期刊:Physics of Fluids
[American Institute of Physics]
日期:2024-05-01
卷期号:36 (5)
被引量:2
摘要
To address the challenge of reducing aerodynamic drag while further enhancing the speed of high-speed trains, this research employs the concept of flow control for the bottom parts and draws inspiration from the front wings of Formula 1 (F1) race cars. Three kinds of two-multistage wing deflectors are designed and systematically analyzed by unsteady Reynolds-averaged Navier–Stokes (URANS) turbulent model. The most suitable design is determined by the single bogie model with a simplified train body. Using the improved delayed detached eddy simulation method, the aerodynamic drag of 1:8 three-car train models with or without two-multistage wing deflector is studied at different operational speeds. The results present the total drag reduction is higher at higher speeds. The reductions of 4.26%, 3.92%, 3.63%, and 3.49% are obtained at the operating speeds of 400, 350, 300, and 200 km/h, respectively. The two-multistage wing deflector desirably improves the flow structure at the bottom of the train, which leads to the reduction of aerodynamic drag and a corresponding reduction in the positive pressure zones within the bogie area. Furthermore, the deflector restricts shedding vortices, effectively narrowing the interference range of airflow under the train, which will provide a potential drag reduction method for the next generation high-speed train.
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