使用正弦多孔物体(SPO)和穿孔多孔物体(PPO)对导电板系统的纳米增强型多槽喷射撞击冷却性能的影响

IF 5.4 2区 工程技术 Q1 ENGINEERING, AEROSPACE Propulsion and Power Research Pub Date : 2024-06-01 DOI:10.1016/j.jppr.2024.05.001
Fatih Selimefendigil , Faiza Benabdallah , Kaouther Ghachem , Hind Albalawi , Badr M. Alshammari , Lioua Kolsi
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引用次数: 0

摘要

电子设备、电池和光伏(PV)模块的热管理冷却系统设计对于提高效率、安全运行和延长产品寿命非常重要。在本研究中,提出了两种不同的冷却系统,它们都采用了纳米增强型多重射流,用于导电面板。本冷却系统可用于电子冷却和光伏组件。喷流冷却系统中使用了穿孔多孔物体(PPO)和正弦多孔物体(SPO)。考虑到物体的不同渗透率值(达西数 (Da) 在 10-6 和 10-1 之间),采用有限体积法进行了二维数值分析。在冷却系统中使用 PPO 时,考虑了圆柱体的数量(1 至 6 个)和圆柱体的大小(0.015 至 0.075 个)。在使用 SPO 时,振幅(在 0.1 和 2 之间)和波数(在 1 和 12 之间)会有所变化。使用含有圆柱形纳米颗粒的氧化铝-水纳米流体作为导热流体。当改变 PPO 的渗透率时,单圆柱体的平均温度大约会升高 3.89 °C,而六圆柱体的平均温度大约会降低 0.57 °C。在渗透率最高的 PPO 情况下,增加气缸的尺寸会导致温度下降 5.3 °C。当改变气缸数时,冷却率变化约为 3.6%。与 SPO 的振幅和渗透率相比,SPO 的波数对冷却性能的提高影响更大。当波数增加到 12 时,平均表面温度下降了 12.4 °C。与不使用多孔物体的喷射撞击冷却参考情况相比,使用 PPO 和 SPO 以及纳米流体可使温度分别下降 12.3 ℃ 和 14.4 ℃。
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Effects of using sinusoidal porous object (SPO) and perforated porous object (PPO) on the cooling performance of nano-enhanced multiple slot jet impingement for a conductive panel system

Cooling system design for thermal management of electronic equipment, batteries and photovoltaic (PV) modules is important for increasing the efficiency, safety operation, and long life span the products. In the present study, two different cooling systems are proposed with nano-enhanced multiple impinging jets for a conductive panel. The present cooling systems can be used in electronic cooling and PV modules. Perforated porous object (PPO) and sinusoidal porous object (SPO) are used in the jet cooling system. 2D numerical analysis using finite volume method is conducted considering different values of permeability of the objects (Darcy number (Da) between 10−6 and 10−1). When PPO is used in the cooling system, number of cylinders (between 1 and 6), and size of the cylinders (between 0.015 and 0.075) are considered. In the case of using SPO, amplitude (between 0.1 and 2) and wave number (between 1 and 12) are varied. Alumina-water nanofluid with cylindrical shaped nanoparticles is used as the heat transfer fluid. When permeability is changed for PPO, the average temperature increases by roughly 3.89 °C for a single cylinder and drops by roughly 0.57 °C for a six-cylinder cases. Increasing the size of the cylinder in the PPO case at highest permeability results in temperature drop of 5.3 °C. When changing the number of cylinders, cooling rate varies by about 3.6%. Wave number of SPO is more influential on the cooling performance enhancement as compared to amplitude and permeability of the SPO. The average surface temperature drops by 12.4 °C when the wave number is increased to 12. As compared to reference case of jet impingement cooling without porous object, using PPO and SPO along with the nanofluid result in temperature drop of 12.3 °C and 14.4 °C.

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来源期刊
CiteScore
7.50
自引率
5.70%
发文量
30
期刊介绍: Propulsion and Power Research is a peer reviewed scientific journal in English established in 2012. The Journals publishes high quality original research articles and general reviews in fundamental research aspects of aeronautics/astronautics propulsion and power engineering, including, but not limited to, system, fluid mechanics, heat transfer, combustion, vibration and acoustics, solid mechanics and dynamics, control and so on. The journal serves as a platform for academic exchange by experts, scholars and researchers in these fields.
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