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Low Drag Automotive Mirrors Using Passive Jet Flow Control

机译:使用被动射流控制的低阻汽车后视镜

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This paper introduces and proves a novel automotive mirror base drag reduction method using passive jet flow control. The new concept is to open an inlet at the front part of the mirror, introduces the airflow via a converging duct, and ejects the jet surrounding the mirror surface at an angle toward the center of the mirror. The jet harnesses the energy from the free stream by jet mixing with the main flow via large coherent structures, entrains the main flow to energize the base flow, reduces the wake size and turbulence fluctuation, and ultimately significantly decreases the drag. Above phenomena are proved by wind tunnel testing with PIV and drag force measurement and CFD large eddy simulation (LES) calculation. Two jet mirrors with different inlet areas are studied. The jet mirror tunnel 1 has a smaller inlet area, and the jet mirror tunnel 2 has a 4.7 times larger inlet area. The wind tunnel testing is only done for the baseline and jet mirror tunnel 1. LES is used to study all the three mirror configurations. Both the wind tunnel testing and LES indicate that the jet mirror tunnel 1 reduces the drag by about 18% with smaller wake width. The LES indicates that the jet mirror tunnel 2 with larger inlet area further reduces the wake and achieves a drag reduction of 39%. This paper is only for proof of the concept and no design optimization is done. It is believed that there is a large room to further reduce the drag with a systematic design optimization.
机译:本文介绍并证明了一种采用被动射流控制的新型汽车后视镜减阻方法。新概念是在镜子的前部打开一个入口,通过会聚导管引入气流,然后将围绕镜子表面的射流以一定角度朝镜子的中心喷射。射流通过大型相干结构与主流进行射流混合,从自由流中吸收能量,带动主流向基础流供能,减小尾流尺寸和湍流波动,并最终显着降低阻力。通过PIV和阻力测量以及CFD大涡模拟(LES)计算的风洞测试证明了上述现象。研究了具有不同入口面积的两个喷射镜。喷射镜通道1具有较小的入口面积,而喷射镜通道2具有4.7倍的较大入口面积。风洞测试仅针对基线和射流镜隧道1进行。LES用于研究所有三种镜面配置。风洞测试和LES均表明射流镜隧道1在较小的尾流宽度下将阻力减小了约18%。 LES表示具有较大入口面积的射流镜通道2进一步减小了尾流,并实现了39%的阻力减小。本文仅用于概念验证,未进行任何设计优化。可以相信,通过系统的设计优化,还有很大的空间可以进一步减少阻力。

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