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Investigation of a highly underexpanded jet with real gas effects confined in a channel: flow field measurements

机译:对频道内限制的实际气体效应的高度曝光缺点的调查:流场测量

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This article describes experiments to investigate the fluid-to-wall interaction downstream of a highly underexpanded jet, with a pressure ratio of 120, confined in a channel. Heat transfer induced by Joule-Thomson cooling, which is a realgas effect in such a configuration, has critical implications on the safety of pressurised gas components. This phenomenon is challenging to model numerically due to the requirement to implement a realgas equation of state, the large range of (subsonic and supersonic) velocities, the high turbulence levels and the near-wall behaviour. An experimental setup with simple geometry and boundary conditions, and with a wide optical access was designed and implemented. It consisted of a high-pressure gas reservoir at controlled temperature and pressure, discharging argon through a nozzle into a square channel. This facility was designed to allow for a steady-state expansion from over 120 bar to atmospheric pressure for over 1 min. The choice of fluid, pressure and temperature regulation system, and the implementation of a high pressure particle seeding system are discussed. The gas dynamics of this flow was then investigated by two separate optical techniques. Schlieren measurements were used to locate the position of the Mach disk, and planar particle image velocimetry (PIV) was used to measure the turbulent velocity field in the regions of lower velocitydownstream. Mie scattering images also indicated the presence of a condensed argon phase in the supersonic region as expected from previous studies on nucleation. The observed location of the sharp interface at the Mach disk was found to be in excellent agreement with the Crist correlation. Rapid statistics were derived from the PIV measurements at 3 kHz. The recirculation zone was found to extend about 4 channel heights downstream, and in the region between 2 and 3 channel heights downstream, a continuous deceleration on the centerline velocity was observed in line with the narrowing of t
机译:本文介绍了研究高度曝光的射流下游的流体与壁相互作用的实验,其中压力比为120,限制在通道中。焦耳汤姆森冷却引起的热传递,这是一种在这种配置中的实际效果,对加压气体组分的安全性具有重要意义。这种现象是在数值上进行模拟的具有挑战性,因为要求实施一个原始状态,大范围(亚音音和超声波)速度,高湍流水平和近壁行为的规定。设计和实施具有简单几何和边界条件的实验设置,并具有宽的光学访问。它包括在受控温度和压力下的高压气体储存器,通过喷嘴将氩气排放到方形通道中。该设施旨在允许从120多个BAR到大气压超过1分钟的稳态扩张。讨论了流体,压力和温度调节系统的选择,以及高压颗粒种子系统的实施。然后通过两个单独的光学技术研究该流动的气体动力学。 Schlieren测量用于定位马赫盘的位置,并且使用平面粒子图像速度(PIV)测量较低速度下降区域中的湍流速度场。 MIE散射图像还表明,从先前的核化学研究中预期的超音区中存在浓缩氩相。发现Mach盘处的尖锐界面的观察到位置与Crist Colrelation非常一致。快速统计来自3 kHz的PIV测量。发现再循环区在下游延伸约4个通道高度,并且在下游的2和3个通道高度之间的区域中,逐渐观察到中心线速度的连续减速,与t的缩小相结合

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