Numerical study on the effect of gravity angle on airborne spray cooling with different coolants

Jiajun Chen , Xiufang Liu , Shengjun Wang , Fuhao Zhong , Mian Zheng , Yu Hou
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Abstract

In spray cooling systems designed for airborne equipment or confined packaging conditions, the angle between the spray direction and gravity, known as the gravity angle, significantly affects cooling performance. This study employed the Euler–Lagrange method to build a numerical model for spray cooling with four commonly used working fluids: R134a, HFE-7100, ethyl alcohol, and water. The study investigated the flow and heat transfer characteristics of spray cooling at different gravity angles. The results show that changes in the gravity angle alter the forces acting on the droplets during movement, promoting the aggregation of small droplets into larger ones, which leads to differences in droplet size distribution. This also causes varying degrees of viscous dissipation, resulting in a decrease in average droplet velocity. A nonzero gravity angle introduces a gravity component along the surface direction, causing asymmetry in the velocity and thickness of the liquid film. The region opposite this component exhibits a low-speed, thick liquid film, while the other side shows a high-speed, thin liquid film. These changes in liquid film flow due to the gravity angle affect heat transfer performance. The effect of the gravity angle varies for different working fluids. When the gravity angle increases from 0° to 180°, for low-viscosity and low-surface-tension fluids, such as R134a and HFE-7100, the maximum surface temperature difference exhibits an M-shaped variation, and the mean temperature remains constant. For high-viscosity and high-surface-tension fluids, such as ethyl alcohol and water, both the maximum temperature difference and mean temperature show a U-shaped variation, with optimal heat transfer performance at a gravity angle of 90°. These differences are attributed to the physical properties of the working fluids, which result in variations in liquid film distribution and energy conversion during the spray-cooling process.
不同冷却剂对重力角对空气喷雾冷却影响的数值研究
在为机载设备或密闭包装条件设计的喷雾冷却系统中,喷雾方向与重力之间的夹角(称为重力角)对冷却性能有显著影响。本研究采用欧拉-拉格朗日方法建立了四种常用工质R134a、HFE-7100、乙醇和水的喷雾冷却数值模型。研究了不同重力角下喷雾冷却的流动和换热特性。结果表明,重力角的变化改变了液滴在运动过程中所受的作用力,促使小液滴聚集成大液滴,从而导致液滴尺寸分布的差异。这也会引起不同程度的粘性耗散,导致平均液滴速度下降。非零重力角沿表面方向引入重力分量,导致液膜的速度和厚度不对称。该组分对面的区域呈现低速厚液膜,而另一侧呈现高速薄液膜。这些由重力角引起的液膜流动变化影响了传热性能。重力角对不同工质的影响是不同的。当重力角从0°增大到180°时,对于R134a、HFE-7100等低粘度、低表面张力流体,最大表面温差呈m型变化,平均温度保持不变。对于高粘度和高表面张力的流体,如乙醇和水,最大温差和平均温度均呈u型变化,在重力角为90°时传热性能最佳。这些差异归因于工作流体的物理性质,这导致了喷雾冷却过程中液膜分布和能量转换的变化。
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