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Numerical study of an original device to generate compressible flow in microchannels

机译:原始设备在微通道中产生可压缩流的数值研究

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摘要

This study is devoted to the design of an experimental device to generate shock waves in a micropipe. Indeed, the recent advances in the microfluidics of gas lead the scientific community to the question of scaling law in supersonic regime. Thus, in this paper, we simulate the flow induced by the opening of a small solenoid valve to know if it is able to generate a minishock wave. This shock wave moving in an intermediate pipe could be transmitted into a micro one. In this work, we focus on the flow in the intermediate pipe and on the properties of the transmitted wave into the microchannel. Three geometry of convergent between intermediate and micropipe are investigated. We have compared the results of our simulation to the classical analytical models dealing with shock tubes. After presenting the geometries of the study case, we give the characteristics of our numerical approach, and then we describe our main results. In a last section, the flow generated by the valve used in free jet regime is described. (C) 2008 American Institute of Physics.
机译:这项研究致力于设计一种在微管中产生冲击波的实验装置。确实,气体微流控技术的最新进展使科学界提出了在超音速状态下缩放定律的问题。因此,在本文中,我们模拟了由小型电磁阀打开而引起的流动,以了解其是否能够产生米肖克波。在中间管道中移动的这种冲击波可以传输到微型管道中。在这项工作中,我们关注中间管道中的流动以及进入微通道的传输波的特性。研究了中间管和微管之间会聚的三种几何形状。我们已将模拟结果与处理冲击管的经典分析模型进行了比较。在介绍了研究案例的几何形状之后,我们给出了数值方法的特征,然后描述了我们的主要结果。在最后一部分中,描述了在自由射流状态下使用的阀所产生的流量。 (C)2008美国物理研究所。

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