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Numerical Drag Reduction of a Ground Vehicle by NACA2415 Airfoil Structured Vortex Generator and Spoiler

机译:Naca2415翼型结构涡流发生器和扰流板的地面车辆的数值阻力减少

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Using of computational fluid dynamics (CFD) have big advanteges for design process components in the automotive industry. Flow structures around vehicle and drag forces can investigate in CFD without producing real size prototype vehicle. The drag force affect fuel efficiency and drivability too. In this study, the drag coefficient of 1/15 scale minibus model was minimizated by NACA 2415 airfoil structured vortex generator and front spoiler in Fluent (R). Flow analyses were performed at the 5 different free stream velocities in the range of 2.8 x 10(5)-6.6 x 10(5) Reynolds numbers, where the dynamic similarity condition was provided. The drag coefficient of base minibus model was 0.415. The C-D coefficient of the model minibus was decreased 10.94 % with original designed NACA 2415 airfoil structured vortex generator in model 1. In total of 22.59 % drag reduction was obtained by designed front spoiler. The effect of this drag reduction on fuel consumption about 6 12 % at high vehicle speeds.
机译:使用计算流体动力学(CFD)在汽车行业中设计工艺组件具有大的优势。车辆和拖曳力周围的流动结构可以在CFD中进行研究,而不产生真实尺寸的原型车辆。拖曳力也影响燃油效率和驾驶性能。在该研究中,Naca 2415翼型结构涡流发生器和流畅(R)的前扰流板最小化了1/15级小巴模型的阻力系数。流动分析在5种不同的自由流速度下进行,其范围为2.8×10(5)-6.6×10(5)雷诺数,其中提供动态相似性条件。基础小巴模型的阻力系数为0.415。 Modebus模型的C-D系数减少了10.94%,原装设计的NACA 2415翼型结构涡流发生器中的型号1.总共通过设计的前扰板获得了22.59%的阻力。这种阻力降低燃料消耗的效果在高车速下约612%。

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