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>Time-Resolved PIV for Space-Time Correlations in Hot Jets
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Time-Resolved PIV for Space-Time Correlations in Hot Jets
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机译:用于热喷气机中时空相关的时间分辨PIV
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摘要
Temporally Resolved Particle Image Velocimetry (TR-PIV) is being used to characterize the decay of turbulence in jet flows a critical element for understanding the acoustic properties of the flow. A TR-PIV system, developed in-house at the NASA Glenn Research Center, is capable of acquiring planar PIV image frame pairs at up to 10 kHz. The data reported here were collected at Mach numbers of 0.5 and 0.9 and at temperature ratios of 0.89 and 1.76. The field of view of the TR-PIV system covered 6 nozzle diameters along the lip line of the 50.8 mm diameter jet. The cold flow data at Mach 0.5 were compared with hotwire anemometry measurements in order to validate the new TR-PIV technique. The axial turbulence profiles measured across the shear layer using TR-PIV were thinner than those measured using hotwire anemometry and remained centered along the nozzle lip line. The collected TR-PIV data illustrate the differences in the single point statistical flow properties of cold and hot jet flows. The planar, time-resolved velocity records were then used to compute two-point space-time correlations of the flow at the Mach 0.9 flow condition. The TR-PIV results show that there are differences in the convective velocity and growth rate of the turbulent structures between cold and hot flows at the same Mach number.
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机译:临时分辨粒子图像测速技术(TR-PIV)用于表征射流中湍流的衰减,这是理解射流声学特性的关键要素。 NASA Glenn研究中心内部开发的TR-PIV系统能够以高达10 kHz的频率采集平面PIV图像帧对。此处报告的数据以0.5和0.9的马赫数以及0.89和1.76的温度比收集。 TR-PIV系统的视野沿50.8毫米直径喷嘴的唇线覆盖了6个喷嘴直径。为了验证新的TR-PIV技术,将0.5马赫的冷流量数据与热线风速测量结果进行了比较。使用TR-PIV在剪切层上测得的轴向湍流轮廓比使用热线风速仪测得的轴向湍流轮廓更细,并且沿喷嘴唇线居中。收集的TR-PIV数据说明了冷射流和热射流的单点统计流量特性的差异。然后将平面的时间分辨速度记录用于在0.9马赫流动条件下计算流动的两点时空相关性。 TR-PIV结果表明,在相同的马赫数下,冷热流之间的湍流结构的对流速度和增长率存在差异。
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