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Particle Image Velocimetry Analysis of the Twin Supersonic Jet Structure and Standing-Wave

机译:双超音速喷射结构和驻波的粒子图像测速分析

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High resolution particle image velocimetry measurements of under-expanded twin-jets are presented. Two nozzle pressure ratios are examined, which are selected due to a change in coupling family indicated by a discontinuous jump in screech frequency. Estimates of the turbulent flow statistics, shear-layer thickness, and shear-layer merge point are provided. The effect of the standing-wave on the velocity field is quantified for the first time. The higher nozzle pressure ratio case shows a strong standing-wave with a mismatch between the shock-cell spacing and standing-wavelength. A very weak standing-wave is observed in the lower pressure case, which more closely matches the shock-cell spacing. A snapshot based proper orthogonal decomposition of the instantaneous velocity fields reveal a symmetric coupling mode for the higher pressure case, which could either be flapping or helical in nature. The lower pressure case provided little evidence for plume coupling belonging to an in-plane oscillation.
机译:提出了扩展不足的双射流的高分辨率粒子图像测速仪测量结果。检查了两个喷嘴压力比,这是由于尖叫声频率的不连续跳跃所表示的联轴器系列的变化而选择的。提供了湍流统计,剪切层厚度和剪切层合并点的估计值。第一次量化了驻波对速度场的影响。喷嘴压力比较高的情况下,显示出很强的驻波,而激波单元间距和驻波波长之间不匹配。在较低压力的情况下,观察到非常弱的驻波,该驻波与激波单元的间距更紧密匹配。基于快照的瞬时速度场的正确正交分解揭示了在较高压力情况下的对称耦合模式,该耦合模式本质上可以是拍动的或螺旋形的。较低压力的情况几乎没有证据表明羽流耦合属于平面内振荡。

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