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首页> 外文期刊>International Journal of Automotive Technology >EXPERIMENTAL STUDY COMPARING RACECAR AERODYNAMIC DOWNFORCE-GENERATING DEVICES USING SCALE MODEL NASCAR COT
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EXPERIMENTAL STUDY COMPARING RACECAR AERODYNAMIC DOWNFORCE-GENERATING DEVICES USING SCALE MODEL NASCAR COT

机译:使用比例模型NASCAR COT比较RACECAR气动降力装置的实验研究

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摘要

The performance and safety of the rear wing and spoiler employed on the National Association of Stock Car Auto Racing (NASCAR) COT (car of tomorrow) racecar are experimentally studied using 10 % scale models in a water channel. Particle image velocimetry is used to qualitatively examine the differences in flow structures between the two downforce-generating devices under 0 and 180-degree yaw cases. The latter is important due to an issue with the COT flipping into the air when at extreme yaw (i.e. during a crash). At zero yaw, it is observed that smaller length scales of the flow structures in the wake of the wing compared to those in the wake of the spoiler, provide more predictable handling for racecars in close proximity and may allow more safe and competitive racing. At 180-degree yaw, it is observed that wake-structure interactions may not allow proper operation of anti-flipping devices (roof flaps) on the winged car. In the extreme yaw case, local flow scales are examined and show much stronger Reynolds number (Re) dependence for the wing than the spoiler.
机译:在水通道中,使用10%比例模型对美国储备汽车赛车协会(NASCAR)COT(未来之车)赛车所采用的后翼和扰流板的性能和安全性进行了实验研究。粒子图像测速仪用于定性检查两个下压力产生装置在0度和180度偏航情况下的流动结构差异。后者之所以重要,是因为在极端偏航时(即在碰撞期间),COT会飞向空中。在零偏航下,观察到与扰流板尾流相比,机翼尾流处的流动结构的长度尺度较小,为靠近的赛车提供了更可预测的操纵,并且可以允许更安全和更具竞争力的比赛。在180度偏航下,观察到尾流与结构的相互作用可能无法使有翼汽车上的防翻转装置(屋顶襟翼)正常运行。在极端偏航情况下,检查了局部流量比例,显示出机翼的雷诺数(Re)依赖性比扰流器强得多。

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