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Experimental investigation of unsteady near wakes of ground vehicle bodies.

机译:地面车身非定常近尾流的实验研究。

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The unsteady near wake behind ground vehicle bodies was investigated to further understand the aerodynamics affecting vehicle fuel consumption and operational safety. A three dimensional bluff body model was mounted above a moving ground belt in a wind tunnel facility to simulate the time dependent, three dimensional near wake flow field generated by trucks, buses, and automobiles.; The velocity field was measured with hot wire anemometry. The time averaged and dynamic pressures on the model base were measured with pressure taps and transducers. Spectral analysis of the velocity and pressure signals identified periodic wake flow structures.; The time averaged near wake contains a ring vortex and is enclosed by shear layers which starts where the model boundary layer separates on the body. At the start of the shear layer, vortex shedding was measured at a dimensionless Strouhal frequency, {dollar}Stsb{lcub}H{rcub} = 1.157.{dollar} As these vortices are convected along the shear layer, their separation distance decreases and vortex pairing occurs, halving the frequency. Pairing continues until the shear layers from the three other sides coalesce at the free stagnation point, which separates the near wake from the developing far wake. At the free stagnation point, the vortices are shed periodically into the far wake. This periodic pulsing causes interaction of the upper and lower portions of the ring vortex and was measured at {dollar}Stsb{lcub}H{rcub} = 0.069.{dollar}; The effects of ground clearance, model aspect ratio, model yaw angle, and ground simulation on the near wake and base pressure distribution were also studied.; The applicability of splitter plates and cavities for vehicle drag reduction was investigated. It was determined from a parametric study of splitter plate lengths and positions that the overall mean base pressure could be raised up to 7 percent. This was accomplished by producing a low velocity region on one side of the plate. A four sided base cavity increased the overall mean base pressure up to 11 percent by reducing the near wake velocity fluctuations up to 50 percent and creating a quiescent body of fluid between the base and the unsteady near wake.
机译:对地面车身后部的非稳态近尾流进行了调查,以进一步了解影响车辆燃油消耗和操作安全的空气动力学。在风洞设施中的移动地带上方安装了三维虚张声势人体模型,以模拟由卡车,公共汽车和汽车产生的时间相关的三维近尾流场。用热线风速仪测量速度场。使用压力分接头和传感器测量模型基础上的平均时间和动态压力。速度和压力信号的频谱分析确定了周期性的尾流结构。接近尾声的平均时间包含一个环形涡旋,并被剪切层包围,剪切层从模型边界层在车身上分离的位置开始。在剪切层开始时,以无量纲的Strouhal频率{涡度} Stsb {lcub} H {rcub} = 1.157测量涡旋脱落。当这些涡流沿剪切层对流时,它们的分离距离减小,并且发生涡旋配对,频率减半。配对继续进行,直到来自其他三个侧面的剪切层在自由停滞点合并在一起,这将近尾与正在发展的远尾分开。在自由停滞点,涡流会定期掉入远​​处。该周期性脉冲引起环涡的上部和下部的相互作用,并在{Stsb {lcub} H {rcub} = 0.069。还研究了离地间隙,模型长宽比,模型偏航角和地面模拟对近尾流和基础压力分布的影响。研究了分隔板和空腔在减少车辆阻力方面的适用性。根据对分隔板长度和位置的参数研究确定,总体平均基准压力可提高到7%。这是通过在板的一侧产生低速区域来实现的。通过将近尾流速度波动降低多达50%,并在基底和不稳定的近尾流之间形成静态的流体体,四边形的基础腔将整体平均基础压力提高了11%。

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