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TURBULENT FLOW MEASUREMENTS AND VISUALIZATIONS OF SUPERSONIC JETS IMPINGING ON A FLAT PLATE AND AN INCLINED PLATE

机译:湍流流动测量和撞击平板上的超音速喷射器的可视化和倾斜板

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This study experimentally investigates the flow characteristics of a high-pressure air jets impinging on a flat plate and an inclined plate with various nozzle-to-plane gaps of 10 mm, 20 mm, and 30 mm. Full-field measurements of flow characteristics in the central plane of the nozzle and near the impinging surface are performed using two-dimensional two-component (2D2C) particle image velocimetry (PIV) technique. This paper presents results from the nozzle pressure ratio (NPR) of 2.11, approximately yielding the sonic jet with Mach number of 1.2. Flow characteristics obtained from the 2D2C-PIV measurements with various spatial gaps are compared and presented. Results including the first- and second-order flow statistics, such as mean velocity and turbulent kinetic energy, and effects of the impinging surface to the flow patterns are investigated. Finally, proper orthogonal decomposition (POD) analysis is applied to reveal the statistically dominant flow structures that capture the highest amount flow kinetic energy and play important roles to the flow dynamics and heat transfers.
机译:本研究通过实验研究撞击平板上的高压空气喷射的流动特性,以及具有10mm,20mm和30mm的各种喷嘴到平面间隙的倾斜板。使用二维双组分(2D2C)颗粒图像速度(PIV)技术进行喷嘴的中心平面和撞击表面附近的流动特性的全场测量。本文提出了喷嘴压力比(NPR)为2.11的结果,大致产生具有1.2的马赫数的声波射流。比较和呈现由具有各种空间间隙的2D2C-PIV测量获得的流动特性。研究结果包括第一和二阶流程统计,例如平均速度和湍流动能,以及撞击表面与流动模式的效果。最后,应用了适当的正交分解(POD)分析来揭示统计上显性的流动结构,该结构捕获最高量的流动动能,并在流动动力学和热传输中起重要作用。

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