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首页> 外文期刊>日本機械学会論文集. B編 >Investigation of Aerodynamic Characteristics of Circular Cylinders under Streamwise Pressure Gradients
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Investigation of Aerodynamic Characteristics of Circular Cylinders under Streamwise Pressure Gradients

机译:流向压力梯度下圆柱的空气动力学特性研究

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摘要

Flows around circular cylinders under streamwise pressure gradients were studied experimen- tally. Pressure distributions on the cylinder surface, frequencies of shedding vortices and wake velocity distributions were obtained under the various pressure gradients. The fundamental charac- teristics of flows around the circular cylinders, such as pressure distributions on the cylinders, angles of separation, pressure drags as well as velocity profiles and turbulence in the wake flows, exhibit remarkable discontinuous changes at a specific value of pressure gradient. The specific pressure gradient, which may be called “critical pressure gradient”, is proved to be around X_cr= (dp/dx)/(ρU~2_0 /2d)≈0.05, independently of Reynolds numbers. The vortex shedding vanishes under the pressure gradient more than X_cr.
机译:对流向压力梯度下圆柱体周围的流动进行了实验研究。在各种压力梯度下,获得了气缸表面的压力分布,涡旋的频率和尾流速度分布。圆柱体周围流动的基本特征,例如圆柱体上的压力分布,分离角度,压力阻力以及尾流中的速度分布和湍流,在特定的压力梯度值下表现出显着的不连续变化。与雷诺数无关,证明了比压力梯度(可以称为“临界压力梯度”)在X_cr =(dp / dx)/(ρU〜2_0/2d)≈0.05左右。涡流脱落在压力梯度下比X_cr消失得更多。

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