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首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >Investigation into the turbulence statistics of installed jets using hot-wire anemometry
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Investigation into the turbulence statistics of installed jets using hot-wire anemometry

机译:使用热线风化测量研究安装喷射器的湍流统计

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This work presents a detailed study of the turbulence flow statistics of a jet mounted with its axis parallel to a rigid flat plate. Hot-wire constant temperature anemometry has been used to measure the single-point and two-point statistics of the axial velocity component at several locations within the jet flow field. Results show that the jet mean flow near the plate surface is subjected to a local acceleration and redirection due to a Coand-type effect. The propagation of these effects downstream of the plate trailing edge is strongly dependent on the plate position. Regarding the velocity fluctuations, the mean turbulence intensity levels are seen to decrease as the radial distance between the jet and surface decreases. Analysis of the single-point power spectral density data on the shear layer close to the plate shows that the reduction in magnitude of the low-frequency content of the energy spectrum is responsible for the decrease in turbulence intensity. Additionally, the characteristic time and length scales computed from two-point measurements reduce as the plate is mounted closer to the jet centre-line. The axial eddy convection velocity is seen to increase in the region of high turbulent kinetic energy in the shear layer adjacent to the surface. Empirical models for turbulence characteristic scales and eddy convection velocity are presented. These findings suggest that both the amplitude and distribution of the jet mixing noise sources are affected when closely installed next to a surface. This paper is a continuation of a recent investigation on the turbulence statistics of isolated jets presented in Proenca (Exp Fluids 60(4):63, 2019).
机译:该工作提出了一种详细研究,该湍流流动统计的速度与其轴线平行于刚性平板安装。热线恒温性低温体已经用于测量射流流场内的若干位置处的轴向速度分量的单点和两点统计。结果表明,由于芯片型效应,板表面附近的射流平均流动对局部加速和重定向进行。这些效应在板后边缘下游的传播强烈地取决于板位置。关于速度波动,观察平均湍流强度水平随着射流和表面之间的径向距离而降低。接近板的剪切层上的单点功率谱密度数据的分析表明,能量谱的低频含量的幅度的幅度降低负责湍流强度的降低。另外,从两点测量计算的特征时间和长度缩放减少随着板的安装靠近喷射中心线。轴向涡流速度被观察到与表面相邻的剪切层中的高湍流动能区域增加。介绍了湍流特性尺度和涡流对流速度的实证模型。这些发现表明,射流混合噪声源的幅度和分布在表面紧密地安装在表面旁边时受到影响。本文是最近关于Proenca中呈现的孤立喷气式飞机的湍流统计的延续(Exp流体60(4):63,2019)。

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