首页> 外文会议>International Congress on Sound and Vibration >NON-DIMENSIONAL PARAMETERS CONTROLLING THE BEHAVIOUR OF OSCILLALTORY FLOWS AROUND STACKS OF PARALLEL PLATES IN THERMOACOUSTIC DEVICES
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NON-DIMENSIONAL PARAMETERS CONTROLLING THE BEHAVIOUR OF OSCILLALTORY FLOWS AROUND STACKS OF PARALLEL PLATES IN THERMOACOUSTIC DEVICES

机译:控制热声器件中的平行板堆叠行为的非维度参数流动

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In thermoacoustic engines and coolers, a compressible fluid undergoes an oscillatory motion around a solid body to facilitate an energy transfer between heat and acoustic waves. The solid body often takes a form of a stack of parallel plates. The oscillatory flow leads to interesting vortex shedding processes at the end of stack, which impacts the performance of the thermoacoustic device due to possible modification of heat transfer processes. There have been many works, experimental and numerical, dedicated to studies of the fluid flow around stacks, both for dimensions representative for realistic devices and using scaled-up arrangements, to obtain a better insight into the flow processes. Depending on the plate thickness, plate spacing and the fluid displacement amplitude, a series of distinct vortex shedding flow patterns are identified. These are either related to a breakup of thin elongated shear layers, or von Karman-like shedding (typical for bluff bodies in steady flows). However, the broad parameter space and the flow physics, which is still not very well understood, make the comparisons between various configurations and flow conditions difficult. Subsequently it is difficult to devise appropriate criteria for the design of stacks. The present work is an effort to find a unified approach to studying the oscillatory flow phenomena around stacks. Firstly, the Navier-Stokes equation is normalized for this particular type of flow, and a group of potential controlling parameters is identified. Secondly, based on the data available from existing literature and our own experiments, the complex phenomena of the oscillatory flow around a stack are discussed in some detail using the likely non-dimensional controlling parameters. Conclusions and suggestions for future work are drawn.
机译:在热声发动机和冷却器中,可压缩流体在固体周围经历振荡运动,以便于热和声波之间的能量转移。固体通常采用一叠平行板的形式。振荡流动导致堆叠末端的有趣的涡流过程,这会影响热声装置的性能,因为可能的传热过程改变。已经有许多作品,实验和数值,致力于研究堆叠周围的流体流动,用于尺寸代表现实设备和使用缩小装置,以获得更好地了解流程过程。取决于板厚度,板间距和流体位移幅度,识别出一系列不同的涡流流动模式。这些是与薄细长剪切层的破碎有关,或者von Karman样脱落(稳定流动的典型虚弱体)。然而,广泛的参数空间和流量物理学仍然不太清楚,使得各种配置和流动条件之间的比较困难。随后难以设计堆叠设计的适当标准。目前的工作是努力寻找统一的方法来研究堆叠周围的振荡流现象。首先,Navier-Stokes方程被归一化为这种特定类型的流量,并且识别了一组电位控制参数。其次,基于现有文献和我们自己的实验可获得的数据,使用可能的非维度控制参数一些细节讨论堆叠周围的振荡流的复杂现象。绘制未来工作的结论和建议。

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