Liang Dandan, Guo Ruichao, Sun Zichun, Zhao Haizhen, Qin Guohua, Zhang Yongxin
School of Aeronautical Engineering, Shandong Engineering Research Center of Aeronautical Materials and Devices, Shandong University of Aeronautics, Binzhou 256600, China.
School of Aeronautical Manufacturing Engineering, Nanchang Hangkong University, Nanchang 330063, China.
Nanomaterials (Basel). 2025 Jan 12;15(2):108. doi: 10.3390/nano15020108.
Spray cooling, of which the essence is droplet impacting, is an efficient thermal management technique for dense electronic components in unmanned aerial vehicles (UAVs). Nanofluids are pointed as promising cooling dispersions. Since the nanofluids are unstable, a dispersant could be added to the fluid. However, the added dispersant may influence the droplet, thereby impacting behaviors. In this work, the effects of dispersant on the nanofluid droplet-impacting dynamics are studied experimentally. The base fluid is deionized water (DI water), and AlO is the selected nanoparticle. Sodium dodecyl sulfate (SDS) is used as the dispersant. Five different concentrations of nanofluids are configured using a two-step method. Droplet impacting behaviors are observed by high-speed imaging techniques. The other effects, i.e., the nanofluid particle volume fraction and the Weber number on droplet impact dynamics, are also systematically investigated. The results illustrate that the surface tension of the AlO nanofluid increases with increased nanofluid concentrations. The surface tension of AlO nanofluid with SDS is lower than that of DI water. And the increase in droplet impact velocity increases the spreading morphology. Nanofluid droplets exhibit spreading and equilibrium process when SDS is added. Furthermore, as the concentration of the nanofluid increases, the spreading process is inhibited. Whereas without SDS, the droplets undergo spreading, receding, and equilibrium processes. Moreover, there is no appreciable change in the impacting process with concentration increase. The empirical models of maximum spreading factor should be established without SDS and with SDS, respectively. This study can provide theoretical basis and specific guidance for experimental characterization of UAVs' electronic devices based on the mechanism of nanofluid droplet impact on the wall.
喷雾冷却的本质是液滴冲击,是一种用于无人机(UAV)中密集电子元件的高效热管理技术。纳米流体被认为是很有前景的冷却分散体。由于纳米流体不稳定,可以向流体中添加分散剂。然而,添加的分散剂可能会影响液滴,进而影响其冲击行为。在这项工作中,通过实验研究了分散剂对纳米流体液滴冲击动力学的影响。基础流体是去离子水(DI水),所选纳米颗粒是AlO。使用十二烷基硫酸钠(SDS)作为分散剂。采用两步法配置了五种不同浓度的纳米流体。通过高速成像技术观察液滴冲击行为。还系统地研究了其他影响因素,即纳米流体颗粒体积分数和韦伯数对液滴冲击动力学的影响。结果表明,AlO纳米流体的表面张力随着纳米流体浓度的增加而增加。添加SDS的AlO纳米流体的表面张力低于DI水。液滴冲击速度的增加会增加铺展形态。添加SDS时,纳米流体液滴呈现铺展和平衡过程。此外,随着纳米流体浓度的增加,铺展过程受到抑制。而不添加SDS时,液滴经历铺展、回缩和平衡过程。而且,随着浓度增加,冲击过程没有明显变化。应分别建立不添加SDS和添加SDS时最大铺展因子的经验模型。本研究可为基于纳米流体液滴冲击壁面机理的无人机电子设备实验表征提供理论依据和具体指导。