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A Study of Impinging Spray G on Transient Thermal Loading and Fuel1 Film Deposition 冲击喷雾 G 对瞬态热加载和燃料1 薄膜沉积的影响研究
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-09-01 DOI: 10.1615/atomizspr.2024054862
Meghnaa Dhanji, Zachary Buen, Logan White, Julien Manin, Lyle Pickett
Under engine cold-start conditions, gasoline injections result in fuel deposition on the cylinder surfaces, due to inhibited fuel vapourisation when the contact surfaces are cold. This can lead to the presence of unburnt hydrocarbons and the formation of soot. The Engine Combustion Network’s (ECN) Spray G impinging on a wall, under various temperature conditions, was investigated using surface temperature measurements a suite of optical diagnostics including Low-Coherence Interferometry (LCI). PACE20 under different injection and ambient temperatures was tested. The measurements reported are of non-reacting conditions, whereby the focus of the study is to analyse spray-wall interaction, prior to flame arrival. The experiments were performed inside a spray vessel under engine-relevant conditions, with sprays impinging on a temperature-controlled wall equipped with nine fast-response, surface thermocouples. The wall was placed 40 mm downstream from the injector to represent the typical distance between the piston surface and injector during cold-start injections in the intake cycle. The injector was mounted on a rotational stage, causing different regions of the plume to impinge on the thermocouple array. This enabled high spatial and temporal resolution of the surface temperature measurements. LCI was used for film thickness quantification, which provided insights on the film dynamics upon impingement and the evaporation rates. High-speed visualisation techniques further aided in the understanding of transient fuel distribution on the wall.
在发动机冷启动条件下,汽油喷射会导致燃料沉积在气缸表面,原因是接触面冷时燃料蒸发受到抑制。这会导致未燃烧碳氢化合物的存在并形成烟尘。发动机燃烧网络 (ECN) 利用表面温度测量和低相干干涉仪 (LCI) 等一系列光学诊断技术,对各种温度条件下撞击壁面的 G 喷雾进行了研究。测试了不同喷射温度和环境温度下的 PACE20。所报告的测量结果是在非反应条件下进行的,因此研究重点是分析火焰到达之前喷壁之间的相互作用。实验是在发动机相关条件下的喷射容器内进行的,喷射物撞击在装有九个快速反应表面热电偶的温控壁上。温控壁位于喷油器下游 40 毫米处,代表进气循环冷启动喷油时活塞表面与喷油器之间的典型距离。喷射器安装在旋转台上,使不同区域的羽流撞击到热电偶阵列上。这使得表面温度测量具有很高的空间和时间分辨率。使用 LCI 对薄膜厚度进行量化,可深入了解薄膜在撞击时的动态和蒸发率。高速可视化技术进一步帮助了解燃料在壁上的瞬时分布。
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引用次数: 0
Application of an Optimized Mechanism of Primary Reference Fuel to Single Hole Sprays 在单孔喷射中应用初级参考燃料的优化机制
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-09-01 DOI: 10.1615/atomizspr.2024051862
Raul Payri, JOSE M GARCIA-OLIVER, Ricardo Novella, Jose M. Pastor, Weiwei Shang, Dario López-Pintor
The present work focuses on the derivation and evaluation of a chemical kinetic mechanism of Primary Reference Fuel (PRF, binary blends of n-heptane and isooctane) with a homogeneous reactors approach starting from a detailed one. Results show that the optimized mechanism can replicate the results of the detailed one with high accuracy. The mechanism is integrated into a Computational Fluid Dynamics workflow combining a Reynolds-Averaged Navier–Stokes approach, a diffuse-interface spray and an unsteady flamelet progress variable combustion models. The workflow is validated against spray combustion measurements following the standards of the Engine Combustion Network (ECN). Test cases sweep binary blends of PRF fuels from pure n-heptane to pure iso-octane using an ECN Spray A nozzle. The model can provide accurate predictions of typical reacting spray metrics such as ignition delay and lift-off length, which have been evaluated following a reconstruction of the experimental methods of schlieren and OH* chemiluminescence. Different definitions of the previous combustion metrics have been compared. The model captures the decreasing reactivity with increasing iso-octane fraction, which results in flame stabilizing at much leaner conditions. However, deficiencies are observed for low reactivity cases, either with high PRF or low temperature cases.
本研究的重点是在详细机制的基础上,采用均相反应器方法推导和评估初级参考燃料(PRF,正庚烷和异辛烷的二元混合物)的化学动力学机制。结果表明,优化后的机理可以高精度地复制详细机理的结果。该机制被集成到计算流体动力学工作流程中,该流程结合了雷诺平均纳维-斯托克斯方法、扩散界面喷雾和非稳态火焰小进变量燃烧模型。按照发动机燃烧网络(ECN)的标准,根据喷雾燃烧测量结果对工作流程进行了验证。测试案例使用 ECN 喷雾 A 喷嘴对从纯正庚烷到纯异辛烷的 PRF 燃料二元混合物进行了扫描。该模型可以准确预测典型的反应喷雾指标,如点火延迟和升空长度,这些指标是通过重构裂片和 OH* 化学发光实验方法进行评估的。对之前燃烧指标的不同定义进行了比较。该模型捕捉到了反应性随异辛烷组分增加而降低的现象,这导致火焰在更稀的条件下趋于稳定。然而,在低反应性情况下,无论是高 PRF 还是低温情况下,都会出现缺陷。
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引用次数: 0
Numerical Investigation of Off-center Collision between Two Equal-sized Water Droplets 两个大小相等的水滴偏离中心碰撞的数值研究
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-08-01 DOI: 10.1615/atomizspr.2024052913
Weidong Yu, Shinan Chang, Shuoshuo Wang
Droplet collision is a basic phenomenon in numerous natural and industrial processes, while the understanding of collision dynamics is still lacking. In this work, a numerical investigation of off-center collision of two equal-sized water droplets is performed with the Weber number of 14 to 196 and impact parameter of 0 to 0.8. The incompressible Navier-Stokes equations are solved by the finite volume method. Volume of Fluid (VOF) method and adaptive mesh technique are used to capture the gas-liquid interface. Firstly, by comparing with reliable published experimental data, the reliability of the numerical results is verified. Then the shape evolution for coalescence, reflexive separation and stretching separation is described detailly. The effect of the Weber number and impact parameter on the collision of two equal-sized water droplets is analyzed. Moreover, the analysis of the surface energy and kinetic energy is conducted for the collision process. Furthermore, the dimensions of ligament and bridge for high impact parameter stretching separation are presented quantitatively. Finally, the collision outcome for the simulation cases in this work is depicted and discussed. This study is helpful for fundamentally understanding the mechanism of collision dynamics of droplets, as well as applying droplet collision model to related processes.
水滴碰撞是众多自然和工业过程中的基本现象,但人们对碰撞动力学的认识仍然不足。在这项工作中,对两个大小相等的水滴在韦伯数为 14 至 196、冲击参数为 0 至 0.8 的条件下的偏心碰撞进行了数值研究。采用有限体积法求解不可压缩的纳维-斯托克斯方程。采用流体体积(VOF)法和自适应网格技术来捕捉气液界面。首先,通过与可靠的公开实验数据进行比较,验证了数值结果的可靠性。然后详细描述了凝聚、反射分离和拉伸分离的形状演变。分析了韦伯数和冲击参数对两个大小相等的水滴碰撞的影响。此外,还分析了碰撞过程中的表面能和动能。此外,还定量给出了高冲击参数拉伸分离时韧带和桥梁的尺寸。最后,对本研究中模拟案例的碰撞结果进行了描述和讨论。这项研究有助于从根本上理解液滴碰撞动力学机理,并将液滴碰撞模型应用到相关过程中。
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引用次数: 0
Derivation of a universal constant set in the Kelvin-Helmholtz Rayleigh-Taylor (KH-RT) breakup model for spray simulations of various fuels 推导用于各种燃料喷雾模拟的开尔文-赫姆霍兹-瑞利-泰勒(KH-RT)破裂模型中的通用常数集
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-08-01 DOI: 10.1615/atomizspr.2024052328
Yanzhi Zhang, Ye Bian, Zonghan Zhang, Zihe Liu, Ming Jia
The Kelvin-Helmholtz Rayleigh-Taylor (KH-RT) breakup model has been extensively utilized in fuel spray simulations. In the KH-RT model, there are five important empirical model parameters, which need to be calibrated carefully for different fuels under various operating conditions. In this work, the global sensitivity analysis of the model constants in the KH-RT breakup model reveals that the model constant for switching the KH and RT mechanisms, Cb, is a dominant parameter affecting the simulation accuracy with the variation of fuel type. To determine the optimal Cb for gasoline spray, the computational fluid dynamics (CFD) program of spray simulation is coupled with the evolutionary genetic algorithm to obtain a quantitative relationship between Cb and ambient density (ρamb). Compared with diesel spray, Cb for gasoline spray is reduced owing to its lower density, viscosity, and surface tension, making it easier for gasoline spray to form smaller droplets after injection. Therefore, the influence of fuel properties should be considered when optimizing Cb. By elucidating the correlation between the physical properties of different fuels and their respective optimal Cb values, this formula is extended to encompass dimethyl ether (DME), biodiesel, and methanol in the present study. The validation results affirm that the enhanced Cb formula effectively reproduces the evolution of the spray for a variety of fuels, aligning well with experimental measurements.
开尔文-赫姆霍兹-瑞利-泰勒(KH-RT)破裂模型已被广泛用于燃料喷雾模拟。在 KH-RT 模型中,有五个重要的经验模型参数,需要针对不同工作条件下的不同燃料进行仔细校准。在这项工作中,对 KH-RT 破裂模型中的模型常数进行的全局敏感性分析表明,随着燃料类型的变化,用于切换 KH 和 RT 机制的模型常数 Cb 是影响模拟精度的主要参数。为了确定汽油喷雾的最佳 Cb,喷雾模拟的计算流体动力学(CFD)程序与进化遗传算法相结合,得到了 Cb 与环境密度(ρamb)之间的定量关系。与柴油喷雾相比,汽油喷雾的 Cb 会降低,这是因为汽油的密度、粘度和表面张力较低,使得汽油喷雾在喷射后更容易形成较小的液滴。因此,在优化 Cb 时应考虑燃料特性的影响。通过阐明不同燃料的物理性质与其各自最佳 Cb 值之间的相关性,本研究将该公式扩展到二甲醚 (DME)、生物柴油和甲醇。验证结果表明,增强型 Cb 公式有效地再现了各种燃料的喷雾演变过程,与实验测量结果十分吻合。
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引用次数: 0
On the role of trancritical evaporation in controlling the transition from two-phase to single-phase mixing 跨临界蒸发在控制两相混合向单相混合过渡中的作用
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-08-01 DOI: 10.1615/atomizspr.2024053690
Grazia Lamanna, Bernhard Weigand, Christoph Steinhausen
The dynamics of near-critical single droplets allows to investigate the transition from two-phase to single-phase mixing under well-defined conditions, devoid of the additional complications due to drop-drop interactions and combustion. Recently, an empirical regime map was proposedto predict the evolution of microscopic transcritical droplets. The experiments show that classical evaporation remains the controlling mechanism over a wide range of supercritical ambient pressures and temperatures with respect to the critical point of the evaporating fluid. Moreover, the onset ambient pressure for the transition to single-phase mixing varies inversely with temperature. To explain this trend, the behavior of a single droplet at near-critical conditions is investigated theoretically by means of a Langmuir-type evaporation model, originally proposed by Young. The model incorporates a modified boundary condition due to the inclusion of gas kinetic effects close to the vapor-liquid interface. This advanced evaporation model is employed to reproduce analytically the above-mentioned regime map, showing a good agreement with experimental findings. The analysis also revealed that the onset of the single-phase mixing regime is associated to the quenching of the evaporation process. The latter is caused by the decrease of the evaporation coefficients, which control the mass transfer rate across the Knudsen layer. The resulting reduction in evaporative cooling leads to the rapid heating of the liquid droplet and to the disintegration of the material interface at the critical temperature.
通过近临界单液滴的动力学研究,可以在明确定义的条件下研究从两相混合到单相混合的过渡,避免了因液滴间相互作用和燃烧而产生的额外复杂性。最近,有人提出了一种经验制度图来预测微观跨临界液滴的演变。实验表明,相对于蒸发流体的临界点,在很宽的超临界环境压力和温度范围内,经典蒸发仍然是控制机制。此外,过渡到单相混合的起始环境压力与温度成反比变化。为了解释这一趋势,我们通过杨最初提出的朗缪尔型蒸发模型,从理论上研究了单个液滴在近临界条件下的行为。由于在汽液界面附近加入了气体动力学效应,该模型包含了一个经过修改的边界条件。利用这一先进的蒸发模型分析再现了上述体系图,显示出与实验结果的良好一致性。分析还显示,单相混合体系的出现与蒸发过程的淬火有关。后者是由蒸发系数的降低引起的,而蒸发系数控制着穿过克努森层的传质速率。蒸发冷却的减少导致液滴迅速升温,材料界面在临界温度下解体。
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引用次数: 0
Effect of flash boiling and air-assisted injection on methanol spray characteristics 闪沸和空气辅助喷射对甲醇喷雾特性的影响
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-07-01 DOI: 10.1615/atomizspr.2024049845
Maohui Su, Jiaqing Ding, Kai Liu, Cangsu Xu, Wenhua Zhou
The advantages of methanol as an alternative fuel have been well demonstrated. However, the difficulty of atomization restricts its practical application. Also, flash boiling and air-assisted injection have been shown to improve the atomization quality of fuels. In this work, the methanol spray characteristics with and without air assistance were experimentally investigated. The experimental conditions include flash-boiling and non-flash-boiling states. High-speed backlight imaging and a Malvern laser particle size analyzer were used to obtain the spray images and droplet sizes, respectively. The flash-boiling state caused a significant variation in spray morphology and the formation of high-concentration central plumes with greater velocity. Compared to the non-flash-boiling spray, the droplet size of the central plumes is larger, whereas the peripheral droplets have a smaller particle size. The droplet size of the air-assisted spray at normal temperature and pressure can reach approximately 3.5 μm, whereas that of the methanol spray without air assistance under a strong flash-boiling state is approximately 60 μm, indicating that air-assisted injection can significantly improve the atomization quality of methanol spray. Furthermore, because of the good atomization, the air-assisted methanol spray is significantly affected by evaporation at high temperatures, and no significant transition of a flash-boiling state was observed.
甲醇作为替代燃料的优势已得到充分证明。然而,雾化困难限制了其实际应用。此外,闪沸和空气辅助喷射已被证明可以改善燃料的雾化质量。本研究通过实验研究了有空气辅助和无空气辅助时的甲醇喷雾特性。实验条件包括闪沸和非闪沸状态。利用高速背光成像仪和马尔文激光粒度分析仪分别获得了喷雾图像和液滴尺寸。闪沸状态导致喷雾形态发生显著变化,并形成速度更快的高浓度中心羽流。与非闪沸喷雾相比,中心羽流的液滴粒径较大,而外围液滴的粒径较小。在常温常压下,空气辅助喷雾的雾滴粒径可达约 3.5 μm,而在强闪沸状态下,无空气辅助的甲醇喷雾的雾滴粒径约为 60 μm,这表明空气辅助喷射可显著改善甲醇喷雾的雾化质量。此外,由于雾化效果良好,空气辅助甲醇喷雾在高温下受蒸发的影响很小,没有观察到明显的闪沸状态转变。
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引用次数: 0
Experimental study on the spray pattern and the merging process of dual-layer rotating conical liquid sheets 双层旋转锥形液片的喷射模式和合并过程的实验研究
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-07-01 DOI: 10.1615/atomizspr.2024052055
Lixin Shen, Shuangcheng Yang, Yangjun Zhang, Weilin Zhuge, Yuping Qian, Zunhua Zhang, Fei Xing
To comprehensively deepen the understanding of the primary breakup mechanism of dual-layer rotating conical liquid sheets, the spray field of a dual-orifice pressure-swirl atomizer was photographed using a high-speed shadowing method. The relationship and mechanism of the influence of the pressure-drop change of primary and pilot flow channels, and dual-layer liquid sheets merging on spray morphology, spray cone angle, and liquid sheet surface fluctuations were investigated in detail based on the analysis of spray field pictures. Attention was focused on the disturbance wave-change mechanism of the dual-layer liquid sheet merging process. The study shows that changing the pressure drop in the primary and pilot flow channels lead to changes in spray pattern, spray cone angle, and liquid sheet surface fluctuations. Furthermore, the influence of pressure drop in the primary flow channel is dominant, and the change in liquid sheet surface fluctuations is related to the spray pattern. In the process of liquid sheet merging (after the inner liquid sheet reaches the expected spray cone angle) the spray cone angle of the outer liquid sheet reduces in size, and only after the dual-layer liquid sheets are in contact with each other do the amplitude of the surface fluctuations of the liquid sheet become significantly larger and generate more medium- and high-frequency scatter.
为全面深化对双层旋转锥形液片一次破裂机理的认识,采用高速阴影法拍摄了双孔压力漩涡雾化器的喷雾场。在分析喷雾场图片的基础上,详细研究了主、先导流道压降变化和双层液片合并对喷雾形态、喷雾锥角和液片表面波动的影响关系和机理。重点研究了双层液片合并过程的扰动波变化机理。研究表明,改变主流道和先导流道中的压力降会导致喷雾模式、喷雾锥角和液面波动的变化。此外,主流道压降的影响占主导地位,液面波动的变化与喷型有关。在液片合并过程中(内层液片达到预期的喷雾锥角后),外层液片的喷雾锥角减小,只有在双层液片相互接触后,液片表面波动的振幅才会明显变大,并产生更多的中频和高频散射。
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引用次数: 0
Acoustic emission of water drops impacting on a heated surface 水滴撞击受热表面的声发射
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-06-01 DOI: 10.1615/atomizspr.2024051683
Volfango Bertola
The sound generated by the impact of water drops on heated surfaces is studied experimentally, with the purpose to identify the sound features characteristic of the various impact morphologies. Whilst the sound of drops impacting on liquid surfaces has been investigated extensively, little attention was given to the sound of drops on solid, heated surfaces. The identification of sound features specific to different impact morphologies would enable the impact regime recognition without the need of high-speed imaging visual inspection, and can be used to train machine learning algorithms for automatic impact regime detection. Water drops were generated from a hypodermic needle suspended above a polished aluminium surface at temperatures between 100°C and 400°C, with impact Weber numbers ranging from 30 to 150. The sound generated upon impact was captured by a supercardioid condenser microphone, and compared with high-speed video recordings of the the impact. Results suggest different impact morphologies generate a sound with distinctive spectral features.
实验研究了水滴撞击受热表面所产生的声音,目的是确定各种撞击形态所特有的声音特征。虽然对水滴撞击液体表面的声音进行了广泛研究,但对水滴撞击固体加热表面的声音却很少关注。识别不同撞击形态所特有的声音特征,可以在不需要高速成像视觉检测的情况下识别撞击状态,并可用于训练自动撞击状态检测的机器学习算法。水滴由悬挂在抛光铝表面上方的皮下注射针头产生,温度在 100°C 至 400°C 之间,撞击韦伯数在 30 至 150 之间。冲击时产生的声音由超心形电容式麦克风捕获,并与冲击的高速视频记录进行比较。结果表明,不同的撞击形态产生的声音具有不同的频谱特征。
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引用次数: 0
Breakup behaviors of annular liquid jet from twin-fluid atomizers in crossflow 横流双流体雾化器环形液体射流的破裂行为
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-05-01 DOI: 10.1615/atomizspr.2024049599
Wenjing XING, Sushil RAUT, Kazunori SATO, Keiya NISHIDA, Yoichi OGATA
This study aims to improve the atomization effect of a liquid jet in crossflow. The atomizer consists of a single injection port, where the liquid and atomizing air are mixed and injected as a two-phase jet. This study used high-speed photographing, image processing, and optical thickness analysis to clarify the breakup mechanism of annular liquid film jets with different properties when they encountered crossflow. The results suggest that the uniformity of liquid film at the atomizer exit strongly dominate the jet breakup process. It was also found that the thickness of the liquid film formed at the exit of the short-mixing port atomizer is non-uniform, whereas the thickness of liquid film produced by the long-mixing port atomizer is relatively uniform, resulting in the spreading of the liquid film jet from the short-mixing port atomizer is larger. Based on the series of experimental results, it can be concluded that the uniformity of the annular liquid film jet is decisive for the atomization state of the two-phase jets in crossflow.
本研究旨在改善横流中液体射流的雾化效果。雾化器由单个喷射口组成,液体和雾化空气在此混合并作为两相射流喷射。本研究采用高速摄影、图像处理和光学厚度分析方法,阐明了不同性质的环形液膜射流在遇到横流时的破裂机理。结果表明,雾化器出口处液膜的均匀性在很大程度上主导着射流的破裂过程。实验还发现,短混合口雾化器出口处形成的液膜厚度不均匀,而长混合口雾化器产生的液膜厚度相对均匀,导致短混合口雾化器的液膜射流扩散量较大。根据这一系列实验结果,可以得出环形液膜射流的均匀性对横流中两相射流的雾化状态起着决定性作用。
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引用次数: 0
Planar two-photon fluorescence imaging of dense spray to estimate spray characteristics: application in pressure-swirl atomizers 对密集喷雾进行平面双光子荧光成像以估计喷雾特性:在压力漩涡雾化器中的应用
IF 1.2 4区 工程技术 Q4 ENGINEERING, CHEMICAL Pub Date : 2024-05-01 DOI: 10.1615/atomizspr.2024052018
Chetankumar Vegad, Said Idlahcen, Longxiang Huang, Gilles Cabot, Bruno Renou, Benjamin Duret, Julien Reveillon, Francois-Xavier Demoulin
The dense spray produced at the primary stage of atomization in a pressure-swirl atomizer is characterized in this work. The optically dense regime from continuous liquid stream to first step breakup into liquid structures is acquired using a two-photon planar laser-induced fluorescence (2p-PLIF) technique. A notable advantage of 2p-PLIF over conventional PLIF is the attenuation of multiple scattering by simultaneous absorption of two photons in an ultra-short pulse duration. This approach is able to capture the complex interface morphology of spray structures. A curvature-based analysis of near-field is carried out to predict far-field spray characteristics. This methodology was recently introduced by cite{Palanti2022} to investigate numerical simulation of atomizing liquid flows. The present work extends its application to experimental images. The atomization process is described through the curvature distribution in different regimes. The spray characteristics are predicted from the early stage of atomization and are reasonably comparable with those of direct measurement by Phase Doppler Anemometry (PDA) in the later stage of atomization. The present analysis shows how it is possible to obtain information about the dispersed phase of the spray in advance based on the dense spray curvature distribution.
本研究对压力漩涡式雾化器在雾化初级阶段产生的致密喷雾进行了表征。采用双光子平面激光诱导荧光(2p-PLIF)技术获取了从连续液流到第一步液体结构破裂的光学致密过程。与传统的 PLIF 相比,2p-PLIF 的一个显著优势是通过在超短脉冲时间内同时吸收两个光子来衰减多重散射。这种方法能够捕捉到喷雾结构复杂的界面形态。通过对近场进行基于曲率的分析,可以预测远场喷雾特性。最近,Palanti 2022 提出了这种方法来研究雾化液体流的数值模拟。本研究将其应用扩展到实验图像。雾化过程是通过不同状态下的曲率分布来描述的。从雾化的早期阶段开始预测喷雾特性,并在雾化的后期阶段与相位多普勒风速仪(PDA)的直接测量结果进行合理比较。本分析表明了如何根据密集喷雾曲率分布提前获得喷雾分散相的信息。
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引用次数: 0
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Atomization and Sprays
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