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首页> 外文期刊>International journal of numerical methods for heat & fluid flow >Cross-sectional reshaping of perturbed/unperturbed rectangular jets
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Cross-sectional reshaping of perturbed/unperturbed rectangular jets

机译:扰动/非扰动矩形射流的横截面整形

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Purpose This study aims to investigate the cross-sectional reshaping in transitioning/starting rectangular jets of aspect ratio 2 under various inlet perturbation conditions at the Reynolds number of Re = UDh/v = 17,750. Design/methodology/approach Large eddy simulation results compared with the phase-locked particle image velocimetry data exhibit the cross-sectional jet deformations from rectangular to rounder shapes. Inflow velocity oscillations are introduced at the fundamental frequency associated with the Kelvin-Helmholtz instability characterized by the spectral analysis of the hotwire data and the linear stability predictions. Findings The initially rectangular cross-section of the jet reshapes into the rounder geometries with increased downstream distance while the edges of the jet become distorted due to the shear layer instability more significantly observed near the high curvature corners. The different expansion rates in the longer and shorter edges of the jet and the consequent cross-sectional reshaping are found to be sensitive to small levels of random inlet perturbations. In addition, introducing controlled sinusoidal oscillations results in the formation of more organized trailing shear layer where the stronger vortex rings go through the curvature-induced deformations. Originality/value Spatio-temporal study of vortex dynamics in transitioning rectangular jets reveals important information about the effect of the controlled jet forcing on local entrainment. Dynamics of the leading vortex dominates the entrainment in transitioning jets which are commonly used in practical applications. Near-field entrainment is also promoted proportional to the amplitude of the controlled inlet oscillations within the trailing vortex rings.
机译:目的本研究旨在研究在雷诺数为Re = UDh / v = 17,750的情况下,在各种入口扰动条件下,长宽比为2的过渡/起始矩形射流中的横截面重塑。设计/方法/方法与锁相颗粒图像测速数据相比,大涡模拟结果显示出横截面射流从矩形变形为圆形。引入速度振荡是在与开尔文-亥姆霍兹不稳定性相关的基频上引入的,其特征是热线数据的频谱分析和线性稳定性预测。研究结果射流的最初矩形横截面随着下游距离的增加而重新成形为更圆的几何形状,而射流的边缘由于在高曲率拐角附近观察到的剪切层不稳定性而变得扭曲。发现喷嘴的较长和较短边缘的不同膨胀率以及随之而来的横截面整形对少量随机入口扰动敏感。另外,引入受控的正弦振荡会导致形成更有组织的尾随剪切层,其中较强的涡旋环会经历曲率引起的变形。独创性/价值时变矩形喷气流中涡流动力学的时空研究揭示了有关受控喷气强迫对局部夹带的影响的重要信息。前涡流的动力学控制着在实际应用中通常使用的过渡射流中的夹带。近场夹带也随尾涡环内受控入口振荡的振幅成比例地促进。

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