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Relative contributions of drag and non-drag forces governing particle motion in pressurized gas-solid jets 在加压气固射流中控制粒子运动的阻力和非阻力的相对贡献
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-01-09 DOI: 10.1016/j.ijmultiphaseflow.2026.105612
Donald E. Peterson, Bradley R. Adams
This study numerically evaluated the relative contributions of drag (FD), fluid stress (FSF), added mass (FAM), and Basset history (FH) forces on particle motion as a function of particle size and gas pressure in a one-dimensional gas-solid jet. The analysis used particle and CO2 gas properties representative of a pilot-scale pressurized oxy-coal combustor inlet at 300 K. Particle diameters of 20-125 μm and gas pressures of 5-40 bar were considered with an inlet velocity of 5 m/s. Force contributions were assessed through force-to-gravity ratios and cumulative force fractions. Results showed that drag was the dominant force beyond the velocity core. However, for larger particles at elevated pressures, FSF and FH locally exceeded FD in regions where gas-particle velocity differences were small. FSF and FAM peaked at the gas velocity gradient discontinuity at the jet core exit, while FH peak lagged this location due to its history effects. FSF and FH were consistently greater than FAM at all conditions. Cumulative force contribution results confirmed that non-drag forces influenced early particle motion for 125 μm particles at 20–40 bar, though their relative importance diminished with distance. Particle velocity responsiveness to changing gas velocity increased with both size and pressure, with non-drag forces most relevant when drag was weak. Findings demonstrate that under high-pressure conditions, forces often considered negligible in atmospheric gas-solid flows may contribute significantly to local particle dynamics.
在一维气固射流中,阻力(FD)、流体应力(FSF)、附加质量(FAM)和巴塞特历史力(FH)对颗粒运动的相对贡献以粒径和气体压力为函数进行了数值计算。该分析使用了代表中试加压氧煤燃烧室进口在300 K时的颗粒和CO2气体特性。考虑颗粒直径为20 ~ 125 μm,气体压力为5 ~ 40 bar,入口速度为5 m/s。通过力与重力比和累积力分数来评估力的贡献。结果表明,在速度核心之外,阻力是主导力。然而,对于高压下较大的颗粒,在气粒速度差较小的区域,FSF和FH局部超过FD。FSF和FAM峰值出现在射流核心出口处的气体速度梯度不连续处,而FH峰值由于其历史影响而滞后于该位置。在所有条件下,FSF和FH均大于FAM。累积力贡献结果证实,在20-40 bar条件下,非阻力力影响125 μm颗粒的早期运动,但其相对重要性随着距离的增加而降低。颗粒速度对气体速度变化的响应性随尺寸和压力的增加而增加,当阻力较弱时,非阻力最相关。研究结果表明,在高压条件下,在大气气固流动中通常被认为可以忽略不计的力可能对局部粒子动力学有重大贡献。
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引用次数: 0
On the modelling of the wall-void layer in high-pressure, subcooled flow boiling 高压过冷流动沸腾中壁面空洞层的模拟
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-01-08 DOI: 10.1016/j.ijmultiphaseflow.2026.105609
Silvia Nauer, Joel-Steven Singh, Djamel Lakehal
In the context of the wall heat flux partitioning approach, we propose a new modelling route for high-pressure, subcooled flow boiling, which we simplify by removing the quenching part. Examining the experimental data used for comparison showed that bubble nucleation at the wall disrupts the boundary layer structure in the same way as wall roughness. We demonstrate that redefining wall friction by linking the roughness length to the bubble departure diameter produces unexpectedly good results. Only when this new model is activated can the boundary layer be correctly recovered. In addition, this work reveals that the lift force should be activated based on fundamental operating conditions such as system pressure, power, mass flux and subcooling, rather than on bubble diameter alone. The aim of this work is not to introduce a universal boiling model, but rather to highlight a few research directions that may provide greater insight into the fundamental mechanisms governing highly convective boiling flows, including the validity of lift forces in this context.
在壁面热流密度划分方法的背景下,我们提出了一种新的高压过冷流动沸腾的建模路线,我们通过去除淬火部分来简化该路线。对比实验数据表明,壁面气泡成核破坏边界层结构的方式与壁面粗糙度破坏边界层结构的方式相同。我们证明,通过将粗糙度长度与气泡离开直径联系起来重新定义壁面摩擦会产生意想不到的好结果。只有激活这个新模型,才能正确地恢复边界层。此外,这项工作还揭示了升力的激活应基于系统压力、功率、质量通量和过冷度等基本运行条件,而不仅仅是气泡直径。这项工作的目的不是介绍一个通用的沸腾模型,而是强调一些研究方向,这些研究方向可以提供对控制高对流沸腾流的基本机制的更深入的了解,包括升力在这种情况下的有效性。
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引用次数: 0
Experimental investigation of secondary atomization in high-speed gas flow 高速气流中二次雾化的实验研究
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-01-08 DOI: 10.1016/j.ijmultiphaseflow.2026.105611
Dajun Xin , Jinhong Liu , Kun Xue
This study develops empirical correlations for the secondary atomization dynamics of water droplets exposed to high-speed flows spanning three orders of Weber number magnitude (We ∼ O(101)–O(103)). It achieves this by employing shock-tube experiments coupled with time-resolved shadowgraph imaging. Over 100 trials resolve the deformation and breakup processes across subsonic to supersonic regimes. Thereby, the cross-stream deformation rates, maximum flattening ratios, and dimensionless breakup initiation times (τb,i) were quantified as functions of We. The results reveal that a two-stage trend in τb,i emerges: a rapid decay below We ∼ 500 transitions to a gradual saturation above We ∼ 1500. This is consistent with a shift in breakup regime dominance from bag-type breakup to shear-induced entrainment. A novel grayscale intensity analysis method isolates the core droplet morphology from the surrounding satellite mist. This enables a precise tracking of the transient mass shedding. Core flattening persists until perimeter shear stripping initiates an exponential mass decay that follows a We-independent scaling law in the shear/ Catastrophic regime. Spatial satellite distributions (resolved via high-resolution digital in-line holography (DIH)) reveal We-dependent shedding mechanisms governed by the transition from bag-type (We ∼ O(101))to transition from bag-type to shear-driven (We ∼ O(102)) and shear-driven breakup (We ∼ O(103)). The transient drag coefficient for the core droplet depends on its aspect ratio, which evolves dynamically with shape deformation and mass shedding. Integrating these correlations for secondary atomization and time-varying drag yields trajectory predictions for core droplet that exhibit deviations less than 7% from experimental data across the tested conditions. This demonstrates the enhanced predictive accuracy of the proposed models over a broad We range.
该研究开发了暴露在高速流动中的水滴的二次雾化动力学的经验相关性,跨越三个韦伯数量级(We ~ O(101) -O(103))。它通过使用激波管实验和时间分辨阴影成像来实现这一目标。超过100次试验解决了亚音速到超音速的变形和破裂过程。因此,横流变形速率、最大扁化比和无因次破碎起始时间(τb,i)被量化为We的函数。结果表明,τb,i出现了两个阶段的趋势:在We ~ 500以下快速衰减,在We ~ 1500以上逐渐饱和。这与破碎机制主导地位的转变是一致的,从袋状破碎到剪切诱导的夹带。一种新的灰度强度分析方法将核心液滴形态从周围的卫星雾中分离出来。这样可以精确地跟踪瞬态质量脱落。岩心扁化一直持续到周长剪切剥离引发指数质量衰减,该衰减遵循剪切/灾难性状态下与we无关的标度定律。空间卫星分布(通过高分辨率数字直线全息(DIH)解析)揭示了We依赖的脱落机制,由从袋型(We ~ O(101))到从袋型到剪切驱动(We ~ O(102))和剪切驱动的破裂(We ~ O(103))的转变所控制。岩心液滴的瞬态阻力系数取决于其长径比,长径比随形状变形和质量脱落而动态变化。将二次雾化和随时间变化的阻力的这些相关性整合在一起,得出了在测试条件下,岩心液滴的轨迹预测与实验数据的偏差小于7%。这证明了所提出的模型在广泛的We范围内具有更高的预测精度。
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引用次数: 0
Physically-based models for predicting the bubbly-to-slug flow transition in vertical downward gas–liquid two-phase flow 垂直向下气液两相流中气泡向段塞流转变的物理模型
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-01-08 DOI: 10.1016/j.ijmultiphaseflow.2026.105610
Abderraouf Arabi, Youssef Stiriba, Jordi Pallares
Accurately predicting flow regime transitions remains one of the key challenges in multiphase flow systems, with significant implications for design, safety, and operational reliability. In this study, novel models are introduced to predict the bubbly-to-slug flow transition in vertical downward gas–liquid flows. The transition to bubbly flow is defined in such a way that it reflects the disappearance of slug-like flow structures, offering a more intuitive physical interpretation of the underlying mechanisms. Two independent and physically meaningful criteria are proposed: (i) the onset of homogeneous flow behavior and (ii) the vanishing of the Taylor bubble. Based on these criteria, analytical expressions are derived using recent correlations for global and slug liquid holdups.
The resulting transition lines are nearly identical, underscoring the internal consistency and robustness of the proposed methodology. The models’ performances were validated against an extensive experimental database from the literature and covering a broad range of pipe diameters (9.53 mm ≤ D≤ 80 mm). They showed excellent agreement with observed transitions in most cases, confirming their predictive accuracy.
准确预测流型转变仍然是多相流系统的关键挑战之一,对设计、安全性和运行可靠性具有重要意义。在本研究中,引入了新的模型来预测气液垂直向下流动中气泡到段塞流的转变。气泡流动的转变反映了段塞状流动结构的消失,为潜在机制提供了更直观的物理解释。提出了两个独立的和物理上有意义的标准:(i)均匀流动行为的开始和(ii)泰勒气泡的消失。基于这些准则,利用最近的全局和段塞液含率相关性推导出解析表达式。所得的过渡线几乎相同,强调了所建议方法的内部一致性和健壮性。模型的性能通过广泛的文献实验数据库进行验证,涵盖了广泛的管径(9.53 mm≤D≤80 mm)。在大多数情况下,他们与观察到的转变表现出极好的一致性,证实了他们预测的准确性。
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引用次数: 0
Curvature analysis of the projections of the 3D liquid structures 三维液体结构投影的曲率分析
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-01-06 DOI: 10.1016/j.ijmultiphaseflow.2026.105607
Longxiang Huang , Benjamin Duret , François-Xavier Demoulin
This study investigates the relationship between three-dimensional liquid structures and their two-dimensional projections using curvature analysis. Liquid structures are generated via a direct numerical simulation (DNS) solver for two-phase flow, and their two-dimensional projections are obtained by accumulating the Volume-of-Fluid field onto a single plane, simulating an imaging process. Curvature analysis is applied to both the three-dimensional data and the projected images across a range of Weber numbers and liquid volume fractions. Representative test cases illustrate the influence of structural superposition within this framework. Results indicate that, despite inherent projection-related biases, the curvature distributions derived from two-dimensional projections effectively capture the morphological characteristics of the original three-dimensional shapes. Key geometric features remain largely consistent across varied flow conditions. This work demonstrates the reliability of curvature-based image post-processing and outlines future pathways for integrating experimental imaging with numerical simulations under a unified curvature-analysis framework.
本文利用曲率分析法研究了三维液体结构与其二维投影之间的关系。通过直接数值模拟(DNS)求解器生成两相流的液体结构,并通过将流体体积场累积到单个平面上,模拟成像过程获得其二维投影。曲率分析应用于三维数据和韦伯数和液体体积分数范围内的投影图像。代表性的测试用例说明了在这个框架内结构叠加的影响。结果表明,尽管存在固有的投影相关偏差,但由二维投影导出的曲率分布有效地捕获了原始三维形状的形态特征。关键的几何特征在不同的流动条件下基本保持一致。这项工作证明了基于曲率的图像后处理的可靠性,并概述了在统一的曲率分析框架下将实验成像与数值模拟相结合的未来途径。
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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 : 2026-01-06 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
Laminar dispersion force effects on two-fluid modelling and simulation of bubble column hydrodynamics 层流色散力对双流体气泡柱流体力学建模与仿真的影响
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2026-01-06 DOI: 10.1016/j.ijmultiphaseflow.2025.105590
Arshia Fazeli , Sander Rhebergen , Nasser Mohieddin Abukhdeir
The two-fluid model (TFM) is foundational for modelling and simulation of dispersed-regime multiphase flows which are pervasive in natural and industrial processes. The TFM provides a coarse-grained representation of complex multiphase flows without explicitly capturing interfaces between phases through the use of volume-, time-, or ensemble-averaging. This results in the benefit of significantly reduced computational complexity but at the cost of increased approximation requiring accurate interphase transfer closures, compared to interface-capturing models. The choice of interphase transfer closures for TFM accuracy has been one of the main foci of past research, which is expansive due to the various multiphase system combinations (e.g. gas dispersed in liquid and liquid dispersed in gas). Recent research using detailed interface-capturing models has shown that the inclusion of a laminar dispersion force in the TFM when modelling bubbly flows both improves physical fidelity and mathematical completeness. In this work, a simulation-based study is performed to determine the effects of including different recently proposed laminar dispersion force models on both numerical stability and physical fidelity of a TFM formulation for gas dispersed in liquid multiphase flows. It includes a formulation of a TFM based on Brennen’s canonical formulation incorporating various recently developed laminar dispersion force closures. Overall, it is shown that inclusion of a laminar dispersion force both improves numerical stability and physical fidelity through validation with past experimental results.
双流体模型(TFM)是对自然和工业过程中普遍存在的分散型多相流进行建模和仿真的基础。TFM提供了复杂多相流的粗粒度表示,而无需通过使用体积、时间或整体平均来明确捕获相之间的界面。与接口捕获模型相比,这样做的好处是大大降低了计算复杂性,但代价是需要更精确的间相转移闭包。选择相间转移闭包以提高TFM精度一直是过去研究的主要焦点之一,由于各种多相系统组合(例如气分散在液中和液分散在气中),这一研究范围很广。最近使用详细界面捕获模型的研究表明,在模拟气泡流动时,在TFM中加入层流色散力既提高了物理保真度,又提高了数学的完整性。在这项工作中,进行了一项基于模拟的研究,以确定包含不同的最近提出的层流分散力模型对气体在液体多相流中分散的TFM公式的数值稳定性和物理保真度的影响。它包括基于Brennen标准公式的TFM公式,该公式结合了各种最近开发的层流色散力闭包。总体而言,通过与以往实验结果的验证,表明层流色散力的加入既提高了数值稳定性,又提高了物理保真度。
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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 : 2026-01-03 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
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 : 2026-01-03 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。
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引用次数: 0
Experimental study of particle-laden turbulent horizontal pipe flows up to Reτ≈ 2000 in the two-way coupling regime 双向耦合状态下Reτ≈2000以下含粒子水平管湍流的实验研究
IF 3.8 2区 工程技术 Q1 MECHANICS Pub Date : 2025-12-30 DOI: 10.1016/j.ijmultiphaseflow.2025.105591
Guanzhe Cui, Adel Emadzadeh, Zhongyu Xu, Jason Monty, Jimmy Philip
<div><div>To understand the effects of particle settling and Reynolds number, experiments are conducted in a smooth-wall horizontal pipe with a diameter <span><math><mrow><mi>D</mi><mo>=</mo><mn>10</mn><mspace></mspace><mi>cm</mi></mrow></math></span>, and using particles of diameter <span><math><mrow><msub><mrow><mi>d</mi></mrow><mrow><mi>p</mi></mrow></msub><mo>=</mo><mn>250</mn><mspace></mspace><mi>μ</mi><mi>m</mi></mrow></math></span> at viscous-scale Stokes numbers of <span><math><mrow><mi>S</mi><msup><mrow><mi>t</mi></mrow><mrow><mo>+</mo></mrow></msup><mo>=</mo><mn>0</mn><mo>.</mo><mn>96</mn></mrow></math></span>–5.93, a volume fraction of <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mi>v</mi></mrow></msub><mo>=</mo><mn>0</mn><mo>.</mo><mn>022</mn><mtext>%</mtext></mrow></math></span>, and a particle-to-fluid density ratio of <span><math><mrow><msub><mrow><mi>ρ</mi></mrow><mrow><mi>p</mi></mrow></msub><mo>/</mo><msub><mrow><mi>ρ</mi></mrow><mrow><mi>f</mi></mrow></msub><mo>=</mo><mn>1</mn><mo>.</mo><mn>05</mn></mrow></math></span>. Measurements of the streamwise and radial velocities of both the fluid and particle phases are obtained using planar imaging techniques (PIV and PTV). Two friction Reynolds numbers, <span><math><mrow><mi>R</mi><msub><mrow><mi>e</mi></mrow><mrow><mi>τ</mi></mrow></msub><mo>≈</mo><mn>850</mn></mrow></math></span> and <span><math><mrow><mn>2</mn><mspace></mspace><mn>050</mn></mrow></math></span>, corresponding to bulk Reynolds numbers of <span><math><mrow><mi>R</mi><msub><mrow><mi>e</mi></mrow><mrow><mi>b</mi></mrow></msub><mo>=</mo><mn>32</mn><mspace></mspace><mn>000</mn></mrow></math></span> and <span><math><mrow><mn>86</mn><mspace></mspace><mn>000</mn></mrow></math></span>, respectively, are studied, along with an additional experimental dataset at <span><math><mrow><mi>R</mi><msub><mrow><mi>e</mi></mrow><mrow><mi>τ</mi></mrow></msub><mo>≈</mo><mn>190</mn></mrow></math></span> with the same <span><math><mrow><msub><mrow><mi>ρ</mi></mrow><mrow><mi>p</mi></mrow></msub><mo>/</mo><msub><mrow><mi>ρ</mi></mrow><mrow><mi>f</mi></mrow></msub></mrow></math></span>. We observe that turbulence modulation depends on <span><math><mrow><mi>R</mi><msub><mrow><mi>e</mi></mrow><mrow><mi>τ</mi></mrow></msub></mrow></math></span> both at the pipe centreline and off-centreline. In general, the streamwise intensity of the fluid phase increases relative to the unladen case, the radial intensity decreases, and the Reynolds stress is reduced. The velocity statistics of the particle phase generally match those of the fluid phase, except for the radial intensity, which is higher for the particles than for the fluid, highlighting the importance of particle settling. To quantify settling due to gravity, we introduce a new non-dimensional number and use it to classify different experiments in channels and pipes. We also perform a drag decomposition, finding that at the highest <span><math><mrow><mi>R</mi><msub><mrow><mi>e</mi></mro
为了解颗粒沉降和雷诺数的影响,在直径D=10cm的光滑壁水平管道中,采用粒径dp=250μm的颗粒,在粘度尺度下Stokes数为St+=0.96 ~ 5.93,体积分数为ϕ =0.022%,粒液密度比为ρp/ρf=1.05。利用平面成像技术(PIV和PTV)测量流体和颗粒相的流向和径向速度。研究了两个摩擦雷诺数Reτ≈850和2050,分别对应于Reb=32000和86000的体积雷诺数,以及Reτ≈190处具有相同ρp/ρf的附加实验数据。我们观察到湍流调制取决于管道中心线和非中心线的Reτ。总的来说,流体相的流向强度相对于空载情况增大,径向强度减小,雷诺应力减小。颗粒相的速度统计基本上与流体相匹配,但颗粒的径向强度高于流体,突出了颗粒沉降的重要性。为了量化重力沉降,我们引入了一个新的无量纲数,并用它来对不同的通道和管道实验进行分类。我们还进行了阻力分解,发现在最高Reτ下,颗粒应力可以贡献10%以上的总阻力。由于我们没有观察到颗粒流中阻力的任何整体变化,分解表明湍流通过雷诺剪切应力的贡献减少,并被颗粒应力所取代,保持大致相同的整体阻力。通过象限分析对雷诺剪应力的详细分析表明,颗粒的引入减少了波及和喷射贡献,并倾向于使象限贡献随机化,有效地降低了整体雷诺剪应力。
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Measurements of the streamwise and radial velocities of both the fluid and particle phases are obtained using planar imaging techniques (PIV and PTV). Two friction Reynolds numbers, &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mi&gt;R&lt;/mi&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;e&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;τ&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;mo&gt;≈&lt;/mo&gt;&lt;mn&gt;850&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt; and &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mn&gt;2&lt;/mn&gt;&lt;mspace&gt;&lt;/mspace&gt;&lt;mn&gt;050&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;, corresponding to bulk Reynolds numbers of &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mi&gt;R&lt;/mi&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;e&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;b&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;mo&gt;=&lt;/mo&gt;&lt;mn&gt;32&lt;/mn&gt;&lt;mspace&gt;&lt;/mspace&gt;&lt;mn&gt;000&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt; and &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mn&gt;86&lt;/mn&gt;&lt;mspace&gt;&lt;/mspace&gt;&lt;mn&gt;000&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;, respectively, are studied, along with an additional experimental dataset at &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mi&gt;R&lt;/mi&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;e&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;τ&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;mo&gt;≈&lt;/mo&gt;&lt;mn&gt;190&lt;/mn&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt; with the same &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;ρ&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;p&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;mo&gt;/&lt;/mo&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;ρ&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;f&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt;. We observe that turbulence modulation depends on &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mi&gt;R&lt;/mi&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;e&lt;/mi&gt;&lt;/mrow&gt;&lt;mrow&gt;&lt;mi&gt;τ&lt;/mi&gt;&lt;/mrow&gt;&lt;/msub&gt;&lt;/mrow&gt;&lt;/math&gt;&lt;/span&gt; both at the pipe centreline and off-centreline. In general, the streamwise intensity of the fluid phase increases relative to the unladen case, the radial intensity decreases, and the Reynolds stress is reduced. The velocity statistics of the particle phase generally match those of the fluid phase, except for the radial intensity, which is higher for the particles than for the fluid, highlighting the importance of particle settling. To quantify settling due to gravity, we introduce a new non-dimensional number and use it to classify different experiments in channels and pipes. We also perform a drag decomposition, finding that at the highest &lt;span&gt;&lt;math&gt;&lt;mrow&gt;&lt;mi&gt;R&lt;/mi&gt;&lt;msub&gt;&lt;mrow&gt;&lt;mi&gt;e&lt;/mi&gt;&lt;/mro","PeriodicalId":339,"journal":{"name":"International Journal of Multiphase Flow","volume":"197 ","pages":"Article 105591"},"PeriodicalIF":3.8,"publicationDate":"2025-12-30","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"145923474","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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