中尺度合成射流的动量场和温度场研究

Omidreza Ghaffari, M. Dogruoz, M. Arik
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引用次数: 3

摘要

由于高传热率,热管理已成为先进微纳米电子系统的关键部分。更多的限制,如紧凑,占地面积小,重量轻,高可靠性,易于使用和低成本暴露给热工程师。先进的电子系统,如笔记本电脑、平板电脑、智能手机和超薄电视系统,都承载着这些具有挑战性的热需求。对于这些设备来说,比以往任何时候都更小的热流密度产生了当前热技术无法轻松满足这些需求的问题。因此,创新的冷却技术是必要的,以满足这些激进的热需求。合成射流是一种很有前途的技术,可以满足这种紧凑电子器件的热需求。合成射流的喷嘴-表面距离对其冷却性能的影响一直没有得到广泛的研究,也没有得到很好的理解。在一些现有的实验研究中,据报道,合成射流的性能对这个距离非常敏感,当射流靠近热表面时,其性能就会下降。因此,我们进行了一项计算研究,以了解射流与表面间距为H/Dh=5时小型合成射流的流动物理特性。空间离散采用二阶迎风格式,时间离散采用二阶隐式格式以保证稳定性。研究发现,喷管出口处的脉动流动会产生涡,而这些涡对目标表面轮廓的影响似乎很小。确定了局部表面压力、速度、湍流分布和换热系数分布,讨论了射流频率和近壁涡的影响。
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An investigation into momentum and temperature fields of a meso-scale synthetic jet
Thermal management has become a critical part of advanced micro and nano electronics systems due to high heat transfer rates. More constraints such as compactness, small footprint area, lightweight, high reliability, easy-access and low cost are exposed to thermal engineers. Advanced electronic systems such as laptops, tablets, smart phones and slim TV systems carry those challenging thermal needs. For these devices, smaller thermal real estates with higher heat fluxes than ever have created issues that current thermal technologies cannot meet those needs easily. Therefore, innovative cooling techniques are necessary to fulfill these aggressive thermal demands. Synthetic jets have been studied as a promising technology to satisfy the thermal needs of such tight electronics devices. The effect of nozzle-to-surface distance for a synthetic jet on its cooling performance has neither been studied extensively nor been well-understood. In a few available experimental studies, it was reported that synthetic jet performance is very sensitive to this distance and when the jet gets closer to the hot surface its performance degrades. Therefore, a computational study has been performed to understand the flow physics of a small-scale synthetic jet for a jet-to-surface spacing of H/Dh=5. Spatial discretization is implemented via a second order upwind scheme and a second order implicit scheme is used for temporal discretization to ensure stability. It is found that pulsating flow at the nozzle exit generates vortices and these vortices seem to have minimal effect on the target surface profiles. Local surface pressure, velocity, turbulence profiles and heat transfer coefficient distributions are determined, then the effects of jet frequency as well as near-wall vortices are discussed.
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