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SPATIAL VELOCITY CORRELATIONS AND NEAR FIELD PRESSURE MEASUREMENTS FROM A HEATED TRANSONIC AXISYMMETRIC JET

机译:跨声速轴对称射流的空间速度相关性和近场压力测量

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摘要

Turbulence properties and the near field pressure of a Mach 0.85 jet at two different static temperature ratios (0.87 and 2.4) are studied. The turbulence properties were studied using PIV measurements which were performed with the light sheet aligned in the radial and the streamwise directions at locations between 3.3 and 8.2 jet diameters downstream from the nozzle exit. Measurements of the near field pressure fluctuations were acquired using a linear array of 6 pressure transducers evenly spaced from 3.45 to 8.45 jet exit diameters. From the PTV measurements it was observed that the heated jet is narrower than the unheated jet and has a higher peak normalized TKE. The highly correlated area of the 2 point spatial velocity correlations is larger for the unheated jet than the heated jet. The measurements from the pressure transducers reveals that the relative amplitude of the mean fluctuating pressure is slightly higher for the heated jet after the end of the potential core. The convection speed of the waves propagating along the pressure sensor array was calculated to be larger for the heated jet.
机译:研究了在两种不同的静态温度比(0.87和2.4)下,马赫数为0.85的射流的湍流特性和近场压力。使用PIV测量研究了湍流特性,该测量是通过将光片在喷嘴出口下游的3.3和8.2喷嘴直径之间的位置沿径向和流向对齐的方式进行的。使用线性阵列的6个压力传感器,其射流出口直径均匀地分布在3.45至8.45之间,获得了近场压力波动的测量结果。从PTV测量中可以看出,加热的喷射流比未加热的喷射流更窄,并且具有更高的归一化TKE峰值。未加热射流的两点空间速度相关性的高度相关区域比加热射流大。压力传感器的测量结果表明,在势芯结束后,受热射流的平均脉动压力的相对幅度略高。对于加热的射流,沿压力传感器阵列传播的波的对流速度计算得较大。

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