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Onset and influencing factors of deflecting oscillation in planar opposed jets

机译:平面对置射流偏转振荡的起因及影响因素

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摘要

The oscillation behaviors of planar opposed jets are experimentally and numerically studied for a Reynolds number range of 16-5000. The flow of planar opposed jets is visualized by some white smoke, and the images of smoke-seeded flow are captured by a 2-D pianar particle imaging veiocimetry (PIV) and a high-speed camera. Effects of the nozzle separation, the exit Reynolds number, the confinement of boundary and the width-to-height ratio of exit on the oscillation behaviors of planar opposed jets are investigated and discussed. Different flow regimes have been identified at various nozzle separations and exit Reynolds numbers. The transition from the stable separated flow to the impingement plane flapping flow and the onset of deflecting oscillation are reported for the first time from experimental results. The map describing the flow regimes of planar opposed jets is presented. Results show that the confinement of boundary and the width-to-height ratio of exit have effects on the deflecting oscillation.
机译:在16-5000的雷诺数范围内,通过实验和数值研究了平面对置射流的振荡行为。平面对置射流的流动通过一些白烟可视化,并且通过2-Pianar粒子成像测速法(PIV)和高速相机捕获了种子播散的烟流图像。研究并讨论了喷嘴间距,出口雷诺数,边界的限制以及出口的宽高比对平面对置射流的振荡行为的影响。在不同的喷嘴间距和出口雷诺数下已确定了不同的流动方式。从实验结果中首次报道了从稳定的分离流向冲击面扑动流的过渡以及偏转振荡的开始。给出了描述平面对置射流流动状态的图。结果表明,边界的限制和出口的宽高比对偏转振动有影响。

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