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Numerical simulation of airblast atomization process with transforming algorithm and breakup models 用变换算法和破碎模型对空气雾化过程进行数值模拟
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-09 DOI: 10.1016/j.ijmultiphaseflow.2026.105615
Xiaoqiang Sun , Hong Yan , Fuzhen Chen
The multi-scale airblast atomization has important influences on the performance of modern aeroengine combustor. In the present work, the airblast atomization under high density, viscosity and velocity contrasts is investigated with a composite simulation strategy. The adaptive mesh refinement is combined with the Eulerian-Lagrangian transforming algorithm as well as breakup models to avoid unacceptable computational costs. The atomization from continuous jet to dispersed droplets is presented and analyzed. It is shown that the computational grid number of simulation without transformation is 1.52 times simulation with combined strategy under inner high-speed shearing condition. Changing shearing position presents different flow characteristics. The outer high-speed swirling gas has large space to develop and interacts with the sheet for a distance 3.6 times the inner high-speed case. Massive vortical structures are demonstrated in the shearing, turbulent and breakup regions. The Proper Orthogonal Decomposition is implemented to extract energetic coherent structures. The first four modes contribute more than 90% of the axial turbulence kinetic energy. The perturbation growth characteristics are monitored and analyzed with linear stability analysis. For the inner high-speed case, the theoretical dominant frequency is 2546.5Hz which agrees with simulation results. For the outer high-speed case, the linear stability analysis gives the trend of perturbation growth correctly. Key parameters determining the atomization performance are discussed. A comprehensive understanding of the two-phase interaction is obtained.
多尺度空气雾化对现代航空发动机燃烧室的性能有着重要的影响。本文采用复合模拟策略,对高密度、高粘度、高速度条件下的空气雾化进行了研究。自适应网格细化与欧拉-拉格朗日变换算法和分解模型相结合,避免了不可接受的计算成本。介绍并分析了连续射流到分散液滴的雾化过程。结果表明,内高速剪切工况下,不进行变换的模拟计算网格数是采用组合策略模拟的1.52倍。改变剪切位置会产生不同的流动特性。外高速旋流气体具有较大的发展空间,与板材的相互作用距离是内高速壳体的3.6倍。在剪切区、湍流区和破碎区均表现出大量的涡旋构造。采用适当的正交分解方法提取能量相干结构。前4种模态贡献了90%以上的轴向湍流动能。用线性稳定性分析对扰动生长特性进行了监测和分析。内高速情况下,理论主导频率为2546.5Hz,与仿真结果吻合。对于外高速情况,线性稳定性分析正确地给出了微扰增长的趋势。讨论了决定雾化性能的关键参数。对两相相互作用有了全面的认识。
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引用次数: 0
Rise of a confined bubble in a wedge 楔子中密闭气泡的上升
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-22 DOI: 10.1016/j.ijmultiphaseflow.2026.105628
Shakib Ahmed , Gretar Tryggvason , Yue Ling
The dynamics of bubbles in confined geometries is a fundamental problem with significant applications. The rise of a bubble in a wedge-shaped channel, with its opening aligned with gravity, is investigated using three-dimensional interface-resolved numerical simulations and a theoretical model. The embedded boundary and geometric volume-of-fluid methods are used to resolve the wedge wall and bubble surface, respectively. The Bond (Bo) and Laplace (La) numbers, along with the wedge angle, fully determine the bubble dynamics. The rising bubble reaches a stationary equilibrium state, where capillary and gravitational forces balance. The equilibrium state depends only on Bo and the wedge angle. The theoretical model predicts that the equilibrium bubble position and height, when normalized by the capillary length, are independent of Bo, while the normalized width increases with Bo. Parametric simulations span a wide range of Bo and La. The Laplace number, varied by changing liquid viscosity, does not affect the equilibrium state but modulates bubble deformation during the rise.
受限几何气泡的动力学是一个具有重要应用的基本问题。利用三维界面解析数值模拟和理论模型,研究了楔形通道中气泡的上升,其开口与重力方向一致。采用嵌入边界法和几何流体体积法分别求解楔形壁面和气泡面。Bond (Bo)和Laplace (La)数与楔角一起决定了气泡动力学。上升的气泡达到静止的平衡状态,毛细力和重力达到平衡。平衡态只取决于Bo和楔角。理论模型预测,当毛细管长度归一化后,平衡气泡的位置和高度与Bo无关,而归一化宽度随着Bo的增加而增加。参数化模拟跨越了Bo和La的广泛范围。随液体粘度变化的拉普拉斯数不影响平衡状态,但在上升过程中调节气泡变形。
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引用次数: 0
Dry-Wet degradation process of unsaturated metamorphic sandstone based on multi-field coupling mechanism: A Case study of the protection of Damaidi rock art 基于多场耦合机制的非饱和变质砂岩干湿降解过程——以大麦地岩画保护为例
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2025-12-30 DOI: 10.1016/j.ijmultiphaseflow.2025.105598
Guopeng Wu , Jiacheng Sui , Zhuohang Tian , Zhijie Zhao , Guanghao Yu , Ruiying Zhang , Qiangqiang Pei , Kai Cui
This study investigates the accelerated deterioration of Damaidi rock art after summer rainfall, revealing the dry-wet degradation mechanisms of metamorphic sandstone. Based on conservation laws of mass, energy, and momentum, as well as unsaturated porous media theory, the Van Genuchten model is applied to describe water infiltration in unsaturated rock. The model accounts for solid matrix and pore fluid compressibility, thermal effects on fluid flow, and water vapor phase changes impacting rock deformation, establishing a coupled thermal-hydro-mechanical (THM) mathematical framework. Using COMSOL Multiphysics, numerical simulations of the dry-wet degradation process were conducted and validated against experimental data, including temperature, volumetric water content, and stress-strain curves. Key findings include: 1) Spatial heterogeneity in temperature and moisture fields, with boundary effects decaying with depth and a linear increase in temperature response lag; 2) Increased secondary porosity leading to a 17.8% rise in water diffusion coefficient by the 5th cycle; 3) Differential strain up to 0.12% from THM coupling, forming microcrack networks. The simulation results match experimental data with an average relative error below 8.2%, verifying the model’s accuracy in representing THM coupling behavior in unsaturated rock. These insights provide a theoretical foundation for understanding the weathering mechanisms of rock art substrates.
研究了夏季降雨后大麦地岩画的加速变质过程,揭示了变质砂岩干湿降解机制。基于质量、能量和动量守恒定律,结合非饱和多孔介质理论,将Van Genuchten模型应用于非饱和岩石中水的入渗。该模型考虑了固体基质和孔隙流体的可压缩性、热效应对流体流动的影响以及水气相变化对岩石变形的影响,建立了热-水-力耦合数学框架。使用COMSOL Multiphysics,对干湿降解过程进行了数值模拟,并根据实验数据进行了验证,包括温度、体积含水量和应力-应变曲线。主要发现包括:1)温度和湿度场的空间异质性,边界效应随深度衰减,温度响应滞后线性增加;2)第5次循环时,次生孔隙度增加,水扩散系数增加17.8%;3)由THM耦合产生的差应变高达0.12%,形成微裂纹网络。模拟结果与实验数据吻合,平均相对误差小于8.2%,验证了模型对非饱和岩石中THM耦合行为的描述准确性。这些见解为理解岩画基质的风化机制提供了理论基础。
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引用次数: 0
Premature transition to supercritical flow with bubbly flow around a circular cylinder 圆柱周围气泡流动过早过渡到超临界流动
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-06 DOI: 10.1016/j.ijmultiphaseflow.2026.105606
Eric Thacher , Céline Gabillet , Bruno Van Ruymbeke , Simo A. Mäkiharju
Vortex induced vibration (VIV) experienced during flow past a cylinder can reduce equipment performance and in some cases lead to failure. Previous studies have shown that the shift in shedding frequency and vibration amplitude under the influence of gas injection at the upper subcritical range can produce a premature shift to supercritical flow (and the drag crisis). To date, the influence of the gas distribution along the cylinder span has not yet been investigated. Time-resolved particle image velocimetry (TR-PIV), proper orthogonal decomposition (POD) and spectral proper orthogonal decomposition (SPOD) of the wake structures, as well as bubble image velocimetry (BIV) are used to assess the flow topology changes under the influence of spanwise uniform and spanwise discontinuous gas injection. We demonstrate that for gas injected along the span of the cylinder, a premature shift to supercritical flow occurs even at volumetric qualities of 0.034%, which is lower than has been previously shown in literature. For gas injected along the central 1.3D of the channel (30% of the channel width), a local transition to supercritical flow occurs at the channel centerline; however, the wake recovers to that of subcritical flow by 3.6D downstream, as mixing occurs with the predominantly single-phase flow to either side of the bubble injection. This downstream transition in the shedding frequency resembles that of single-phase dual step cylinders, which to the author’s knowledge has not yet been shown to occur under two-phase conditions. At two-phase supercritical flow, for ReD = 360,000, we demonstrate a significant shift in near-wake gas motion and vortex shedding frequency, with gas motion driven by vortex interaction in the separated shear layer.
当流体流过气缸时,所经历的涡激振动(VIV)会降低设备的性能,在某些情况下会导致故障。前人的研究表明,在亚临界上部范围内,受注气影响的脱落频率和振动幅值的变化会导致过早转向超临界流动(以及阻力危机)。到目前为止,还没有研究过沿气缸跨的气体分布的影响。采用时间分辨粒子图像测速(TR-PIV)、尾迹结构适当正交分解(POD)和光谱适当正交分解(SPOD)以及气泡图像测速(BIV)等方法,对沿展向均匀注气和沿展向不连续注气影响下的流动拓扑变化进行了评价。我们证明,对于沿圆柱体跨度注入的气体,即使在体积质量为0.034%时也会过早转向超临界流动,这比先前文献中所显示的要低。沿通道中心1.3D(通道宽度的30%)注入的气体,在通道中心线发生局部向超临界流动过渡;然而,在下游3.6D时,尾迹恢复到亚临界流动的尾迹,这是因为气泡喷射两侧以单相流为主的混合发生了。这种脱落频率的下游转变类似于单相双阶气缸,据作者所知,尚未显示在两相条件下发生。在两相超临界流动中,当ReD = 360,000时,我们发现近尾迹气体运动和旋涡脱落频率发生了显著变化,气体运动是由分离剪切层中的旋涡相互作用驱动的。
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引用次数: 0
Liquid interface dynamics at primary breakup in close-coupled gas atomization 紧密耦合气体雾化初破时的液界面动力学
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-03 DOI: 10.1016/j.ijmultiphaseflow.2025.105596
T. Cheng , R. Leibovici , B. Kong , R. van Hout
Detailed measurements of the liquid jet interface dynamics close to the nozzle exit in close-coupled gas atomization focused on “filming” and “no-filming” conditions and their transitional behavior, were performed using digital inline holography. Experiments covered four Weber numbers, Weg, three apex angles, θ, for a range of momentum flux ratios, M. The JPDFs of the instantaneous liquid jet interface positions revealed strikingly different interface behavior depending on the combination of Weg, M, and θ. A spectral analysis identified coherent axial frequency bands, associated with the radial movement of the jet interfaces. Based on analysis of (i) reconstructed snapshots, (ii) JPDFs of instantaneous jet positions, and (iii) spectral analysis, four different “flow” regimes were proposed, namely “no-filming”, “filming”, and two transitional regimes (“periodic flapping” and intermittent “switching”). Flow regime maps (Rel versus Weg) constructed for different apex angles, show that “filming” occurred at low Rel for all investigated Weg. Increasing θ, increased the value of Rel for which transitional behavior was observed. In addition, keeping M constant while increasing Weg (implies increasing Rel) may cause transition from “filming” to “no-filming”. Despite the different proposed flow regimes, peak Strouhal numbers mostly ranged between 2 Stp 3, irrespective of M, Weg, and θ (excluding “no-filming” conditions). This study has provided a detailed spectral characterization of the transition to filming in CCGA, quantitatively expressed as regime maps that are essential for predicting primary breakup behavior and optimizing atomizer design.
采用数字内嵌全息技术,对紧耦合气体雾化中靠近喷嘴出口的液体射流界面动力学进行了详细测量,重点研究了“成膜”和“无成膜”条件及其过渡行为。在动量通量比M的范围内,采用了4个韦伯数Weg, 3个顶点角θ。不同的Weg、M和θ组合,液体射流的瞬时界面位置的jpdf显示出明显不同的界面行为。光谱分析确定了与射流界面径向运动有关的相干轴向频带。基于(i)重建快照、(ii)瞬时射流位置的jpdf和(iii)光谱分析,提出了四种不同的“流动”模式,即“无拍摄”、“拍摄”和两种过渡模式(“周期性扑动”和间歇性“切换”)。根据不同顶点角度构建的流态图(Rel与Weg)显示,在所有被调查的Weg中,“成膜”都发生在低Rel。θ越大,Rel值越高,出现过渡行为。另外,在保持M不变的同时增加Weg(意味着增加Rel),可能导致从“拍摄”到“不拍摄”的过渡。尽管提出了不同的流动形式,峰值斯特罗哈尔数大多在2≤Stp≤3之间,与M、Weg和θ无关(不包括“无膜”条件)。该研究提供了CCGA中向成膜过渡的详细光谱特征,定量表达为状态图,这对于预测初级破裂行为和优化雾化器设计至关重要。
{"title":"Liquid interface dynamics at primary breakup in close-coupled gas atomization","authors":"T. Cheng ,&nbsp;R. Leibovici ,&nbsp;B. Kong ,&nbsp;R. van Hout","doi":"10.1016/j.ijmultiphaseflow.2025.105596","DOIUrl":"10.1016/j.ijmultiphaseflow.2025.105596","url":null,"abstract":"<div><div>Detailed measurements of the liquid jet interface dynamics close to the nozzle exit in close-coupled gas atomization focused on “filming” and “no-filming” conditions and their transitional behavior, were performed using digital inline holography. Experiments covered four Weber numbers, We<span><math><msub><mrow></mrow><mrow><mi>g</mi></mrow></msub></math></span>, three apex angles, <span><math><mi>θ</mi></math></span>, for a range of momentum flux ratios, <span><math><mi>M</mi></math></span>. The JPDFs of the instantaneous liquid jet interface positions revealed strikingly different interface behavior depending on the combination of We<span><math><msub><mrow></mrow><mrow><mi>g</mi></mrow></msub></math></span>, <span><math><mi>M</mi></math></span>, and <span><math><mi>θ</mi></math></span>. A spectral analysis identified coherent axial frequency bands, associated with the radial movement of the jet interfaces. Based on analysis of (i) reconstructed snapshots, (ii) JPDFs of instantaneous jet positions, and (iii) spectral analysis, four different “flow” regimes were proposed, namely “no-filming”, “filming”, and two transitional regimes (“periodic flapping” and intermittent “switching”). Flow regime maps (Re<span><math><msub><mrow></mrow><mrow><mi>l</mi></mrow></msub></math></span> versus We<span><math><msub><mrow></mrow><mrow><mi>g</mi></mrow></msub></math></span>) constructed for different apex angles, show that “filming” occurred at low Re<span><math><msub><mrow></mrow><mrow><mi>l</mi></mrow></msub></math></span> for all investigated We<span><math><msub><mrow></mrow><mrow><mi>g</mi></mrow></msub></math></span>. Increasing <span><math><mi>θ</mi></math></span>, increased the value of Re<span><math><msub><mrow></mrow><mrow><mi>l</mi></mrow></msub></math></span> for which transitional behavior was observed. In addition, keeping <span><math><mi>M</mi></math></span> constant while increasing We<span><math><msub><mrow></mrow><mrow><mi>g</mi></mrow></msub></math></span> (implies increasing Re<span><math><msub><mrow></mrow><mrow><mi>l</mi></mrow></msub></math></span>) may cause transition from “filming” to “no-filming”. Despite the different proposed flow regimes, peak Strouhal numbers mostly ranged between 2 <span><math><mo>≤</mo></math></span> St<span><math><mrow><msub><mrow></mrow><mrow><mi>p</mi></mrow></msub><mo>≤</mo></mrow></math></span> 3, irrespective of <span><math><mi>M</mi></math></span>, We<span><math><msub><mrow></mrow><mrow><mi>g</mi></mrow></msub></math></span>, and <span><math><mi>θ</mi></math></span> (excluding “no-filming” conditions). This study has provided a detailed spectral characterization of the transition to filming in CCGA, quantitatively expressed as regime maps that are essential for predicting primary breakup behavior and optimizing atomizer design.</div></div>","PeriodicalId":339,"journal":{"name":"International Journal of Multiphase Flow","volume":"197 ","pages":"Article 105596"},"PeriodicalIF":3.8,"publicationDate":"2026-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145923476","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
On the application of refractive index matching to study the buoyancy-driven motion of spheres 折射率匹配在球浮力驱动运动研究中的应用
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-03 DOI: 10.1016/j.ijmultiphaseflow.2025.105597
Jibu Tom Jose , Aviel Ben-Harosh , Omri Ram
Refractive index matching (RIM) is a powerful tool for multiphase flow studies, as it suppresses optical distortions and enables high-fidelity tomographic measurements near solid–fluid interfaces of freely moving solids. However, by improving the RIM and optical quality, the solids become effectively invisible, preventing direct identification of their location. To address this limitation, we develop a physics-informed detection framework that locates transparent spheres in time-resolved tomographic Particle Tracking Velocimetry by combining tracer density field, vertical velocity field, and vortex structures into a unified optimization problem. Integrated with volumetric reconstructions, the method provides simultaneous analysis of velocity, pressure, and force on the sphere. Applied to three acrylic spheres with diameters of 7.93, 9.53, and 11.11 mm, rising in a sodium-iodide RIM solution, the measurements capture both vortex shedding around the sphere and the evolution of the wake, showing distinct regime change between the larger sphere and the smaller ones. The smaller spheres are predominantly coupled to vortex shedding occurring close to them, while the larger sphere motion is closely related to the evolution of coherent vortices in the wake. The technique allows, for the first time, to directly calculate the drag and lift histories on a freely moving sphere over half an oscillation cycle. The framework can be extended to dynamic masking for improved tomographic reconstruction and pressure-field calculations, to non-spherical bodies with more complex motions, and to multi-body interactions, advancing RIM from a flow-only diagnostic to a tool for fully coupled body–wake measurements.
折射率匹配(RIM)是多相流研究的有力工具,因为它可以抑制光学畸变,并在自由移动的固体的固-液界面附近实现高保真层析测量。然而,通过提高RIM和光学质量,固体变得有效地不可见,防止直接识别它们的位置。为了解决这一限制,我们开发了一个物理信息检测框架,通过将示踪剂密度场、垂直速度场和涡旋结构结合到一个统一的优化问题中,在时间分辨层析粒子跟踪速度测量中定位透明球体。该方法与体积重建相结合,可以同时分析球体上的速度、压力和力。应用于三个直径分别为7.93、9.53和11.11 mm的丙烯酸球,在碘化钠溶液中上升,测量结果捕捉到球体周围的漩涡脱落和尾迹的演变,显示出大球体和小球体之间明显的状态变化。较小的球体主要与附近发生的涡脱落耦合,而较大的球体运动与尾迹中相干涡的演变密切相关。该技术首次允许直接计算半个振荡周期内自由运动球体的阻力和升力历史。该框架可以扩展到动态掩蔽,以改进层析成像重建和压力场计算,更复杂运动的非球形物体,以及多体相互作用,将RIM从仅用于流动诊断的工具推进到完全耦合体-尾迹测量的工具。
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引用次数: 0
A novel phase-field lattice Boltzmann method moving contact line model with soluble surfactants 一种新的相场晶格玻尔兹曼方法与可溶性表面活性剂的移动接触线模型
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-09 DOI: 10.1016/j.ijmultiphaseflow.2026.105608
Liping Yao , Peiyu Wang , Liangqi Zhang , Zhong Zeng , Li Li , Shouyong xie
This paper proposes a novel moving contact line model for two-phase flows containing soluble surfactants in the context of phase-field based lattice Boltzmann method (PF-LBM). The model combines a dynamic contact angle model accounting for contact line velocity with the generalized Navier boundary condition (GNBC) based on the phase-field (PF) method to capture the wetting dynamics. In this model, one LB equation solves the Navier-Stokes equations, and two others solve the two Cahn-Hilliard-like equations. A modified chemical potential is incorporated into the LBM framework, and the corresponding equilibrium distribution functions are reformulated simultaneously. First, we evaluate the reliability of the PF-LB model developed in this study by simulating a static droplet suspended in an ambient flow field and the bilateral shear problem of a single droplet. Subsequently, the proposed PF-LBM moving contact line model is extended to droplet spreading dynamics on solid surfaces. The match of the results obtained and the reference solution validates the model’s reliability. Finally, the PF-LBM moving contact line model is employed to investigate the shearing behavior of soluble surfactant-laden droplets on solid surfaces, focusing on the influences of the effective capillary number and surfactant concentration. The simulation results reveal that both the effective capillary number and the surfactant concentration significantly impact the shear wetting behavior of droplets. Holding other parameters constant, an increase in either the effective capillary number or surfactant concentration enhances the droplet deformation.
本文提出了一种基于相场晶格玻尔兹曼方法(bf - lbm)的含可溶性表面活性剂两相流的移动接触线模型。该模型将考虑接触线速度的动态接触角模型与基于相场法的广义Navier边界条件(GNBC)相结合,以捕捉润湿动力学。在该模型中,一个LB方程求解Navier-Stokes方程,另外两个LB方程求解两个Cahn-Hilliard-like方程。在LBM框架中加入了一个修正的化学势,并同时重新表述了相应的平衡分布函数。首先,我们通过模拟悬浮在环境流场中的静态液滴和单个液滴的双边剪切问题来评估本研究中建立的PF-LB模型的可靠性。随后,将所提出的PF-LBM运动接触线模型推广到固体表面上液滴扩散动力学。计算结果与参考解吻合,验证了模型的可靠性。最后,采用PF-LBM移动接触线模型研究了负载表面活性剂的可溶性液滴在固体表面上的剪切行为,重点研究了有效毛细数和表面活性剂浓度的影响。模拟结果表明,有效毛细数和表面活性剂浓度对液滴的剪切润湿行为有显著影响。在保持其他参数不变的情况下,有效毛细数或表面活性剂浓度的增加都会增强液滴的变形。
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引用次数: 0
Collision coalescence study through the dynamics of impinging spray jets 基于碰撞射流动力学的碰撞聚结研究
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-09 DOI: 10.1016/j.ijmultiphaseflow.2026.105613
Ariel Sharon, Yeshayahou Levy
Cloud droplet growth is known to occur through a combination of condensation and collision-coalescence processes. While gravitational collision-coalescence becomes significant for droplets larger than approximately Φ80 μm, and condensation dominates for smaller sizes, a notable gap exists in the intermediate size range of Φ30 – Φ80 μm. In this regime, known as the "condensation-coalescence bottleneck," neither mechanism sufficiently explains the observed rapid droplet growth. To address this gap, the present experimental study investigates droplet dynamics within sprays to simulate the coalescence behavior seen in cloud environments. Focusing on the low Weber number regime, we explore water droplet interactions and growth mechanisms in the Φ5 – Φ80 μm size range, where collision-coalescence may play a crucial but is less understood. Using Vibrating Mesh Piezoelectric Atomizers (VMA) in an impinging, non-reactive spray configuration, we aim to provide new insights into the efficiency and dynamics of droplet growth, contributing to a better understanding of microphysical cloud processes.
已知云滴的生长是通过凝结和碰撞合并过程的结合而发生的。当液滴大于Φ80 μm时,重力碰撞-聚并作用显著,当液滴小于Φ30 μm时,以凝结作用为主,而在Φ30 - Φ80 μm的中间尺寸范围内则存在明显的间隙。在这种被称为“凝聚-聚结瓶颈”的情况下,两种机制都不能充分解释观察到的液滴快速生长。为了解决这一差距,本实验研究调查了喷雾中的液滴动力学,以模拟云环境中所见的聚结行为。聚焦于低韦伯数体系,我们探索了Φ5 - Φ80 μm尺寸范围内的水滴相互作用和生长机制,其中碰撞聚结可能起着至关重要的作用,但鲜为人知。使用振动网格压电雾化器(VMA)在撞击,非反应性喷雾配置中,我们的目标是为液滴生长的效率和动力学提供新的见解,有助于更好地理解微物理云过程。
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引用次数: 0
Effective viscosity closures for dense suspensions in CSP systems via lubrication-enhanced DNS and numerical viscometry 通过润滑增强型DNS和数值粘度测量,为CSP系统中的密集悬浮液提供有效的粘度封闭
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-14 DOI: 10.1016/j.ijmultiphaseflow.2026.105618
Raphael Münster, Otto Mierka, Dmitri Kuzmin, Stefan Turek
Dense particle suspensions are promising heat transfer fluids for next-generation Concentrated Solar Power (CSP) receivers, enabling operating temperatures above 800 °C. However, accurate modeling of the rheological behavior of granular flows is essential for reliable computational fluid dynamics (CFD) simulations. In this study, we develop and assess numerical methodologies for simulating dense suspensions pertinent to CSP applications. Our computational framework is based on Direct Numerical Simulation (DNS), augmented by lubrication force models to resolve detailed particle–particle and particle–wall interactions at volume fractions exceeding 50%. We conducted a systematic series of simulations across a range of volume fractions to establish a robust reference dataset. Validation was performed via a numerical viscometer configuration, permitting direct comparison with theoretical predictions and established benchmark results. Subsequently, the viscometer arrangement was generalized to a periodic cubic domain, serving as a representative volume element for CSP systems. Within this framework, effective viscosities were quantified independently through wall force measurements and energy dissipation fitting. The close agreement between these two approaches substantiates the reliability of the results. Based on these findings, effective viscosity tables were constructed and fitted using polynomial and piecewise-smooth approximations. These high-accuracy closure relations are suitable for incorporation into large-scale, non-Newtonian CFD models for CSP plant design.
致密颗粒悬浮液是下一代聚光太阳能(CSP)接收器很有前途的传热流体,可实现800°C以上的工作温度。然而,精确的颗粒流动流变行为建模对于可靠的计算流体动力学(CFD)模拟至关重要。在这项研究中,我们开发和评估数值方法来模拟与CSP应用相关的密集悬浮液。我们的计算框架基于直接数值模拟(DNS),并辅以润滑力模型,以解决体积分数超过50%时颗粒-颗粒和颗粒-壁的详细相互作用。我们在一系列体积分数范围内进行了系统的一系列模拟,以建立一个强大的参考数据集。通过数值粘度计配置进行验证,允许与理论预测和建立的基准结果进行直接比较。随后,将粘度计的排列推广到周期三次域,作为CSP体系的代表性体积单元。在此框架下,有效粘度通过壁力测量和能量耗散拟合独立量化。这两种方法之间的密切一致证实了结果的可靠性。基于这些发现,构建了有效粘度表,并使用多项式和分段光滑近似进行拟合。这些高精度的闭合关系适用于CSP电厂设计的大型非牛顿CFD模型。
{"title":"Effective viscosity closures for dense suspensions in CSP systems via lubrication-enhanced DNS and numerical viscometry","authors":"Raphael Münster,&nbsp;Otto Mierka,&nbsp;Dmitri Kuzmin,&nbsp;Stefan Turek","doi":"10.1016/j.ijmultiphaseflow.2026.105618","DOIUrl":"10.1016/j.ijmultiphaseflow.2026.105618","url":null,"abstract":"<div><div>Dense particle suspensions are promising heat transfer fluids for next-generation Concentrated Solar Power (CSP) receivers, enabling operating temperatures above 800<!--> <!-->°C. However, accurate modeling of the rheological behavior of granular flows is essential for reliable computational fluid dynamics (CFD) simulations. In this study, we develop and assess numerical methodologies for simulating dense suspensions pertinent to CSP applications. Our computational framework is based on Direct Numerical Simulation (DNS), augmented by lubrication force models to resolve detailed particle–particle and particle–wall interactions at volume fractions exceeding 50%. We conducted a systematic series of simulations across a range of volume fractions to establish a robust reference dataset. Validation was performed via a numerical viscometer configuration, permitting direct comparison with theoretical predictions and established benchmark results. Subsequently, the viscometer arrangement was generalized to a periodic cubic domain, serving as a representative volume element for CSP systems. Within this framework, effective viscosities were quantified independently through wall force measurements and energy dissipation fitting. The close agreement between these two approaches substantiates the reliability of the results. Based on these findings, effective viscosity tables were constructed and fitted using polynomial and piecewise-smooth approximations. These high-accuracy closure relations are suitable for incorporation into large-scale, non-Newtonian CFD models for CSP plant design.</div></div>","PeriodicalId":339,"journal":{"name":"International Journal of Multiphase Flow","volume":"197 ","pages":"Article 105618"},"PeriodicalIF":3.8,"publicationDate":"2026-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145974416","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Integral equation for translating, vaporizing droplet 蒸发液滴的平移积分方程
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-03-01 Epub Date: 2026-01-19 DOI: 10.1016/j.ijmultiphaseflow.2026.105621
William A. Sirignano
We analyze the unsteady heating and vaporization of a liquid droplet moving through a hot gas. Following the Abramzon–Sirignano reduced-order model, we account for a quasi-steady gas-phase boundary layer and an unsteady liquid-phase heating with the internal circulating convective transport represented through a circulation factor χ. The major aim is to bypass the finite-difference solution of the liquid-phase partial differential heat equation and save computational resources by developing and using a Droplet Integral Method that, through a history integral, yields the surface temperature as a function of time in the Lagrangian tracking of the droplet. Thereby, it provides sufficient information for the two-way coupling of the phases at lower cost. An approximation is introduced to facilitate the creation of a Green’s function to serve as the integral kernel; the approximation is justified by comparison with finite-difference solutions for the internal heating. The potential computational consequences for spray computations are identified and discussed. Liquid heating rate can vary significantly during droplet deceleration relative to the surrounding gas. The Stefan convection and internal liquid circulation significantly modify heating and vaporization rates. Under common constraints, although heat is continually entering at the droplet surface, vaporization rate can increase, then decrease while internal droplet circulation velocity decreases. Meanwhile, droplet radius continually decreases. For accelerating ambient gas, the relative droplet velocity can reverse direction with the droplet Reynolds number first decreasing to zero followed by later increases. In the reversing case, circulation can decrease followed by an increase.
本文分析了液滴在高温气体中运动时的非定常加热和汽化过程。根据abramzon - siignano降阶模型,我们考虑了准稳定气相边界层和非定常液相加热,其中内部循环对流输运通过循环因子χ表示。主要目的是通过开发和使用液滴积分方法,绕过液相偏微分热方程的有限差分解,节省计算资源,该方法通过历史积分,在液滴的拉格朗日跟踪中产生表面温度作为时间的函数。因此,它以较低的成本为相位的双向耦合提供了充分的信息。引入近似是为了方便创建格林函数作为积分核;通过与内加热的有限差分解的比较,证明了近似的正确性。对喷雾计算的潜在计算结果进行了识别和讨论。液滴相对于周围气体减速时,液体加热速率会发生显著变化。Stefan对流和内部液体循环显著地改变了加热和蒸发速率。在一般约束条件下,虽然热量不断从液滴表面进入,但汽化速率会先增大后减小,而液滴内部循环速度会减小。同时,液滴半径不断减小。环境气体加速时,液滴的相对速度发生反向变化,液滴雷诺数先减小到零,后增大。在相反的情况下,循环可以先减少后增加。
{"title":"Integral equation for translating, vaporizing droplet","authors":"William A. Sirignano","doi":"10.1016/j.ijmultiphaseflow.2026.105621","DOIUrl":"10.1016/j.ijmultiphaseflow.2026.105621","url":null,"abstract":"<div><div>We analyze the unsteady heating and vaporization of a liquid droplet moving through a hot gas. Following the Abramzon–Sirignano reduced-order model, we account for a quasi-steady gas-phase boundary layer and an unsteady liquid-phase heating with the internal circulating convective transport represented through a circulation factor <span><math><mi>χ</mi></math></span>. The major aim is to bypass the finite-difference solution of the liquid-phase partial differential heat equation and save computational resources by developing and using a Droplet Integral Method that, through a history integral, yields the surface temperature as a function of time in the Lagrangian tracking of the droplet. Thereby, it provides sufficient information for the two-way coupling of the phases at lower cost. An approximation is introduced to facilitate the creation of a Green’s function to serve as the integral kernel; the approximation is justified by comparison with finite-difference solutions for the internal heating. The potential computational consequences for spray computations are identified and discussed. Liquid heating rate can vary significantly during droplet deceleration relative to the surrounding gas. The Stefan convection and internal liquid circulation significantly modify heating and vaporization rates. Under common constraints, although heat is continually entering at the droplet surface, vaporization rate can increase, then decrease while internal droplet circulation velocity decreases. Meanwhile, droplet radius continually decreases. For accelerating ambient gas, the relative droplet velocity can reverse direction with the droplet Reynolds number first decreasing to zero followed by later increases. In the reversing case, circulation can decrease followed by an increase.</div></div>","PeriodicalId":339,"journal":{"name":"International Journal of Multiphase Flow","volume":"197 ","pages":"Article 105621"},"PeriodicalIF":3.8,"publicationDate":"2026-03-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"146023354","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
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International Journal of Multiphase Flow
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