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Three-dimensional flow structure in highly buoyant jet by scanning stereo PIV combined with POD analysis

机译:立体PIV结合POD分析的高浮力射流三维流动结构

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The flow characteristics and the structure of highly buoyant jet of low density fluid issuing into a stagnant surrounding of high density fluid is studied by scanning stereo My combined with proper orthogonal decomposition (POD) analysis. The experiment is carried out at Froude number of 0.3 and Reynolds number of 200, which satisfies the inflow condition due to the unstable density gradient near the nozzle exit. An increase in the maximum mean velocity occurs and the vertical velocity fluctuation is highly amplified near the nozzle exit, which suggests the influence of inflow due to the unstable density gradient. The POD analysis indicates that the vertical velocity fluctuation is the major source of fluctuating energy contributing to the development of the highly buoyant jet. The examination of the POD modes show that the longitudinal structure of the vertical velocity fluctuation is generated along the jet axis having the opposite sign of velocity fluctuation on both sides of the jet axis. The vertical scale of the POD mode decreases with increasing the mode number and results in the frequent appearance of cross-flow across the buoyant jet. The reconstruction flow from the POD modes indicates that the vortex structure is caused by the highly sheared layer between the upward and downward velocity and the inflow is induced by the vortex structure. The magnitude of the vortex structure seems to be weakened with an increase in the distance from the nozzle and the buoyant jet approaches to an asymptotic state in the further downstream. (C) 2014 Elsevier Inc. All rights reserved.
机译:通过扫描立体My结合适当的正交分解(POD)分析,研究了低密度流体释放到高密度流体停滞周围的流动特性和高浮力射流的结构。实验在0.3的Froude数和200的雷诺数下进行,由于喷嘴出口附近的密度梯度不稳定,因此可以满足流入条件。最大平均速度增加,并且垂直速度波动在喷嘴出口附近高度放大,这表明由于不稳定的密度梯度而导致的流入影响。 POD分析表明,垂直速度波动是能量波动的主要来源,有助于产生高浮力射流。对POD模式的检查表明,垂直速度波动的纵向结构是沿着射流轴生成的,在射流轴的两侧都有相反的速度波动符号。 POD模式的垂直比例随模式数量的增加而减小,并导致频繁出现跨浮力射流的错流。来自POD模式的重构流表明,旋涡结构是由向上和向下速度之间的高剪切层引起的,而流入是由旋涡结构引起的。涡流结构的强度似乎随着与喷嘴的距离的增加而减弱,并且浮力射流在更下游逐渐接近渐近状态。 (C)2014 Elsevier Inc.保留所有权利。

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