Experimental study on Ahmed’s body drag coefficient

IF 0.2 Q4 ENGINEERING, GEOLOGICAL
D. Wysocki, A. Szymanek
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引用次数: 1

Abstract

The work presents an experimental designation of the aerodynamic drag coefficient for two configurations of the Ahmed body model, with slant angle of 25o and with the inactive synthetic jet generator. When analyzing the aerodynamic drag of vehicles, most authors focus on higher Reynolds numbers, describing lower values only by designated trend lines. Which is why the main contribution of this experimental work was to designate the Ahmed’s body drag coefficient for low Reynolds numbers and to verify the obtained results with other authors experiments especially with the trend lines for Reynolds number in the range 0,35x105 – 1,8x105. For data taken from the literature, it can be seen that the value of the drag coefficient for the Ahmed body model decreases when the Reynolds number increases. The results obtained during the experiment show the opposite tendency.
Ahmed体阻力系数的实验研究
本文给出了斜角为250度和不使用合成射流发生器两种构型艾哈迈德模型气动阻力系数的实验设计。在分析车辆的气动阻力时,大多数作者关注的是较高的雷诺数,而较低的雷诺数只能用指定的趋势线来描述。这就是为什么这项实验工作的主要贡献是指定了低雷诺数的艾哈迈德体阻力系数,并与其他作者的实验验证了所获得的结果,特别是在0.35 × 105 - 1.8 × 105范围内的雷诺数趋势线。从文献数据可以看出,Ahmed体模型的阻力系数值随着雷诺数的增加而减小。在实验中得到的结果显示出相反的趋势。
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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来源期刊
Archives for Technical Sciences
Archives for Technical Sciences ENGINEERING, GEOLOGICAL-
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