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Experimental investigation of the flow structures in the wake of a cross parachute canopy

机译:降落伞降落伞尾流后流动结构的实验研究

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In the present study, an experimental study was conducted to characterize the flow structures in the turbulent wake of a cross parachute canopy by utilizing Stereoscopic Particle Image Velocimetry (StereoPIV) technique. Both flow through gap and flow over arm of the cross parachutes were carefully measured and analyzed. The obtained results showed that the turbulent wake of the flow through gap was larger than that of flow over arm. Besides, the distributions of velocity, vorticity, and Reynolds stress of flow through gap differed significantly with those of flow over arm. In addition, the effect of the arm ratio of the cross canopy on the transverse profiles of velocity, vorticity, and Reynolds stress was also discussed. (C) 2016 Elsevier Masson SAS. All rights reserved.
机译:在本研究中,进行了一项实验研究,以通过利用立体粒子图像测速技术(StereoPIV)来表征横降伞机盖的湍流尾流中的流动结构。仔细测量并分析了流经间隙的流量和横降伞上臂的流量。获得的结果表明,流经间隙的湍流比流经臂的湍流更大。此外,通过间隙的流速,旋涡和雷诺应力的分布与通过手臂的流速的分布有显着差异。此外,还讨论了交叉冠层的臂长比对速度,涡度和雷诺应力的横向分布的影响。 (C)2016 Elsevier Masson SAS。版权所有。

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