Numerical Investigation on Enhanced Aerodynamic Performance of a Bus using Vortex Generators - Air Tab and Shark Fin

Raadha Krishnan, Mekala Sanmitra, P. Saravanan, V. Madhanrai, L. Shankaralingam, S. Sivamani
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Abstract

3D flow structures around bus models are computationally analyzed to understand the influence of vortex generator on bus body aerodynamics. The aerodynamics of a vehicle are extremely important since they influence the vehicle's overall performance. As the vehicle is moving on the road, various forces act on an automobile, such as drag and lift force, is a part of vehicle aerodynamics research. One of the primary causes of aerodynamic drag for automobiles is the flow separation at the vehicle's rear end. It is feasible to improve fuel economy by lowering the drag force. This research uses five identical bus models, four with VGs and one without. The purpose is to examine the effects of two types of vortex generators (Air-tab and Shark-fin) in terms of drag coefficient (Cd) and flow pattern developments by mounting the VGs at the rear end of the bus. The flow around the vehicle is considered to be incompressible. It is calculated using the incompressible Reynolds Navier-Stokes equations and k-ε turbulence model. Base Bus model, bus with top Shark-fin VG, bus with top Air-tab VG, bus with Shark-fin VG on 3 sides, bus with Air-tab VG on 3 sides. During the analysis, the bus is subjected to various inlet velocity ranges, ranging from 25m/s to 50 m/s, with an interval of 5m/s. The simulation results show a 7.898% reduction in coefficient of drag (Cd) from the bus model with Air tab vortex generators on 3 sides at 25 m/s.
涡发生器-空气片和鱼翅增强客车气动性能的数值研究
通过对客车模型周围的三维流动结构进行计算分析,了解涡发生器对客车车身空气动力学的影响。汽车的空气动力学非常重要,因为它影响着汽车的整体性能。当车辆在道路上行驶时,作用在汽车上的各种力,如阻力和升力,是车辆空气动力学研究的一部分。汽车气动阻力产生的主要原因之一是汽车尾部的气流分离。通过降低阻力来提高燃油经济性是可行的。这项研究使用了五种相同的巴士模型,四种有VGs,一种没有。目的是通过在客车的后端安装涡发生器,来检验两种涡发生器(Air-tab和Shark-fin)在阻力系数(Cd)和流型发展方面的影响。飞行器周围的气流被认为是不可压缩的。它是用不可压缩雷诺-纳维-斯托克斯方程和k-ε湍流模型计算的。基础总线模型,顶部鲨鱼鳍VG的总线,顶部空气标签VG的总线,3面鲨鱼鳍VG的总线,3面空气标签VG的总线。在分析过程中,母线受到不同的入口速度范围,从25m/s到50m /s,间隔为5m/s。仿真结果表明,在25 m/s速度下,与三面安装Air tab涡发生器的母线模型相比,阻力系数降低了7.898%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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