纳米铝颗粒尺寸和浓度对纳米流体燃料燃烧特性的影响:实验与模拟

IF 3.4 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE Acta Astronautica Pub Date : 2025-01-01 Epub Date: 2024-11-17 DOI:10.1016/j.actaastro.2024.11.030
Shuai Zhou, Jiangong Zhao, Zilong Zhao, Hongjun Liu, Wen Ao
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引用次数: 0

摘要

纳米流体燃料因其提高燃烧特性、能量密度和点火性能的潜力而受到广泛关注。该研究全面考察了不同尺寸(50 nm、100 nm、200 nm、500 nm、1 μm)和不同浓度(2.5 wt%、5.0 wt%、7.5 wt%)的铝纳米颗粒对纳米流体燃料液滴点火和燃烧特性的影响,并利用含有煤油、铝颗粒和表面活性剂油酸的铝基纳米流体燃料溶液进行机械混合。纳米流体燃料液滴的燃烧过程包括点火、稳定燃烧、微爆炸和凝聚反应四个阶段。纳米流体燃料液滴的表面温度始终高于纯煤油液滴,温度升高与颗粒浓度呈正相关,而与颗粒大小无关。含有7.5 wt%铝颗粒的纳米流体燃料液滴的表面温度约为205℃。油酸掺入纯煤油后,点火延迟时间由0.317 s延长至0.333 s。纳米流体燃料液滴的燃烧速率随着铝颗粒的加入而增大,且随着铝颗粒直径和浓度的增加而增大。含有5.0 wt%铝和5.0 wt%油酸颗粒的纳米流体燃料液滴的燃烧速率与纯煤油液滴相似,分别为0.596和0.604 mm2 s−1。同时,纳米流体燃料液滴的点火延迟时间比纯煤油长,但对颗粒大小不敏感。添加7.5 wt%铝颗粒的纳米流体燃料液滴的点火延迟时间约为煤油的1.5倍。不含油酸的纳米流体燃料液滴由于颗粒团聚效应而产生不同的结果。随后,随着颗粒大小的增加,燃烧残渣表面出现更明显的凸起,变得更容易破裂。最后,提出了考虑液滴内部非均匀性的动力学预测模型。点火延迟时间、燃烧速率和稳定表面温度的均方根误差均在8%以下,表明模型预测与实验数据具有很强的相关性。这项研究可能有助于加速铝基纳米流体燃料的采用。
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Effect of aluminum nanoparticles size and concentration on the combustion characteristics of nanofluid fuel: Experiments and modeling
Nanofluid fuel has garnered significant attention due to its potential to enhance combustion characteristics, energy density, and ignition properties. The study comprehensively examined the effects of aluminum nanoparticles with diverse sizes (50 nm, 100 nm, 200 nm, 500 nm, 1 μm) and concentrations (2.5 wt%, 5.0 wt%, 7.5 wt%) on the ignition and combustion characteristics of nanofluid fuel droplets, utilizing a mechanically mixed aluminum-based nanofluid fuel solution that incorporated kerosene, aluminum particles, and the surfactant oleic acid. The combustion process of the nanofluid fuel droplets encompasses phases of ignition, steady combustion, micro-explosion, and agglomerate reaction. The surface temperature of the nanofluid fuel droplets consistently exceeded that of a pure kerosene droplet, with temperature elevations correlating positively with particle concentration but not with the particle size. The surface temperature of nanofluid fuel droplets containing 7.5 wt% aluminum particles is approximately 205°C. The incorporation of oleic acid into pure kerosene prolongs the ignition delay from 0.317 s to 0.333 s. The combustion rate of the nanofluid fuel droplets escalates upon the addition of aluminum particles, with the rate escalating in tandem with the diameter and concentration of the aluminum particles. Nanofluid fuel droplets containing 5.0 wt% aluminum and 5.0 wt% oleic acid particles exhibit a combustion rate akin to that of pure kerosene droplets, with rates of 0.596 and 0.604 mm2 s−1, respectively. Concurrently, the ignition delay for nanofluid fuel droplets is longer than that of pure kerosene, yet it exhibits insensitivity to particle size. The ignition delay for nanofluid fuel droplets with the addition of 7.5 wt% aluminum particles is approximately 1.5 times that of kerosene. Nanofluid fuel droplets devoid of oleic acid yield divergent results due to particle agglomeration effects. Subsequently, as particle size increased, the surface of combustion residue develops more pronounced bulges, becoming more prone to rupture. Ultimately, a kinetic prediction model is proposed, accounting for the inhomogeneous properties within the droplet. The root mean squared errors for ignition delay time, combustion rate, and steady surface temperature are all below 8 %, indicating a strong correlation between model predictions and experimental data. This research could help accelerate the adoption of aluminum-based nanofluid fuel.
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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