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首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >Flow and mixing characteristics of swirling double-concentric jets subject to acoustic excitation
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Flow and mixing characteristics of swirling double-concentric jets subject to acoustic excitation

机译:受声激发的双同心旋流射流的流动和混合特性

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Characteristic flow modes, flow evolution processes, jet spread width, turbulence properties, and dispersion characteristics of swirling double-concentric jets were studied experimentally. Jet pulsations were induced by means of acoustic excitation. Streak pictures of smoke flow patterns, illuminated by a laser-light sheet, were recorded by a high-speed digital camera. A hot-wire anemometer was used to digitize instantaneous velocity instabilities in the flow. Jet spread width was obtained through a binary edge identification technique. Tracer-gas concentrations were measured for information on jet dispersions. Two characteristic flow patterns were observed: (1) synchronized vortex rings appeared in the low excitation intensity regime (the excitation intensity less than one) and (2) synchronized puffing turbulent jets appeared in the high excitation intensity regime (the excitation intensity greater than one). In the high excitation intensity regime, the "suction back" phenomenon occurred and therefore induced in-tube mixing. The jet spread width and turbulent fluctuation intensity exhibited particularly large values in the high excitation intensity regime at the excitation Strouhal numbers smaller than 0.85. At the excitation Strouhal numbers >0.85, the high-frequency effect caused significant decay of jet breakup and dispersion-the jet spread width and fluctuation intensity decreased sharply and may, at very high Strouhal numbers, asymptotically approach values almost the same as the values associated with unexcited jets. Exciting the jets at the high excitation intensity regime, the effects of puffing motion and in-tube mixing caused breakup of the jet in the near field and therefore resulted in a small Lagrangian integral time and small length scales of fluctuating eddies. This effect, in turn, caused drastic dispersion of the central jet fluids. It is possible that the excited jets can attain 90 % more improvements than the unexcited jets. We provide a domain regarding excitation intensity and Strouhal number to facilitate identification of characteristic flow modes.
机译:实验研究了旋流双同心射流的特征流动模式,流动演化过程,射流扩展宽度,湍流特性和弥散特性。喷射脉动是通过声激发引起的。高速数码相机记录了由激光灯照亮的烟雾流动模式的条纹图像。使用热线风速仪将流中的瞬时速度不稳定性数字化。射流散布宽度是通过二进制边缘识别技术获得的。测量了示踪气体的浓度,以获得喷射分散液的信息。观察到两个特征性的流动模式:(1)在低激发强度状态下出现同步涡流环(激发强度小于1)和(2)在高激发强度状态下出现同步膨化湍流射流(激发强度大于1)。 )。在高激发强度条件下,发生“吸回”现象,因此引起管内混合。在激发斯特劳哈尔数小于0.85时,在高激发强度条件下,射流扩展宽度和湍流波动强度表现出特别大的值。在激发斯特劳哈尔数> 0.85时,高频效应导致射流破裂和弥散的明显衰减-射流扩散宽度和波动强度急剧下降,并且在非常高的斯特劳哈尔数下,可能渐近地接近与相关值相同用兴奋的喷气机。在高激发强度条件下激发射流,膨化运动和管内混合的影响导致射流在近场处破裂,因此导致较小的拉格朗日积分时间和较小的涡旋长度尺度。反过来,这种效应导致中央喷射流体的急剧分散。激发的射流比未激发的射流可以获得90%的改善。我们提供了有关激发强度和Strouhal数的域,以便于识别特征流模式。

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