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Experimental study of the motion and shape of a vapor bubble rising in an annular channel at subatmospheric pressure 亚大气压下环形通道中上升的蒸汽泡的运动和形状的实验研究
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060082
R. A. Dekhtyar, V. V. Ovchinnikov

Experimental study was performed for the dynamics of vapor bubble rising in the annular channel at subatmospheric pressure. The gas bubble is formed during boiling of superheated degassed liquid in an annular channel restricted by two glass tubes with the diameters of 25 and 16 mm. It was demonstrated that the dynamics of vapor cavity while rising the vapor bubble in the annular channel demonstrates a qualitative difference from the dynamics for an ascending gas bubble. The behavior is similar to a Taylor vapor bubble behavior in a round tube with a small diameter. One of typical features of vapor cavity behavior in an annular channel is the possibility of vapor cavity decay after the bubble collapse during the pulsation flow mode.

对亚大气压下环形通道中蒸汽气泡上升的动力学进行了实验研究。气泡是过热脱气液体在由两根直径分别为 25 毫米和 16 毫米的玻璃管限制的环形通道中沸腾时形成的。实验证明,环形通道中气泡上升时的蒸汽腔动力学与上升气泡的动力学有本质区别。其行为类似于小直径圆管中的泰勒气泡行为。环形通道中蒸汽腔行为的典型特征之一是,在脉动流模式下,气泡崩溃后蒸汽腔可能会衰减。
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引用次数: 0
Numerical simulation of gas dynamics of the inflow into a channel located behind a conical or plane shock wave 位于锥形或平面冲击波后方的通道流入气体动力学数值模拟
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060045
V. I. Zvegintsev, I. I. Mazhul

The paper presents the results of a numerical study of gas dynamics and integral parameters of the flow at the channel entrance located behind a conical or plane shock wave. The freestream Mach number range is M = 2–4 and the range of the angles of the compression surfaces of the wedge and cone is δ= 10–90°. Data on the flow structure at the channel entrance, mass-averaged Mach numbers, total pressure loss coefficient, and flow rate coefficients are obtained. A comparative analysis of these parameters is performed, and the advantages and drawbacks of the channel entrance positions in various types of the flow are noted.

本文介绍了位于锥形或平面冲击波后面的通道入口处的气体动力学和流动积分参数的数值研究结果。自由流马赫数范围为 M = 2-4,楔形和锥形压缩面的角度范围为 δ= 10-90°。获得了通道入口处的流动结构、质量平均马赫数、总压力损失系数和流速系数等数据。对这些参数进行了比较分析,并指出了在不同类型的流动中通道入口位置的优缺点。
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引用次数: 0
Laws of the monodispersed bubble cluster ascent in a viscous liquid in the presence of surfactant 在有表面活性剂的粘性液体中单分散气泡团上升的规律
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060094
V. A. Arkhipov, A. S. Usanina, R. A. Churkin

The paper presents the results of experimental study for rising a cluster of monodispersed gas bubbles in viscous liquid with/without surfactant for the Reynolds number in the range Re = 0.01–1. The influence of the surfactant type on the dynamics of bubble cluster rising has been analyzed. The qualitative pattern of monodispersed bubble cluster rising was defined as a function of initial void fraction in the range CV = 0.001–0.04. New experimental data were obtained on velocity and drag coefficient for a compact cluster made of monodispersed bubbles rising in a liquid with/without surfactant (both for contact and contactless type of bubble rising).

本文介绍了在雷诺数为 Re = 0.01-1 的范围内,有/无表面活性剂的粘性液体中单分散气泡簇上升的实验研究结果。研究分析了表面活性剂类型对气泡簇上升动力学的影响。在 CV = 0.001-0.04 的范围内,将单分散气泡簇上升的定性模式定义为初始空隙率的函数。在有/无表面活性剂(接触式和非接触式气泡上升)的液体中,获得了由单分散气泡组成的紧凑气泡团上升速度和阻力系数的新实验数据。
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引用次数: 0
The influence of scale factor on simulation results for flow around buildings 比例系数对建筑物周围水流模拟结果的影响
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S086986432306015X
D. A. Dekterev, A. S. Lobasov, V. D. Meshkova, K. Yu. Litvintsev, Ar. A. Dekterev, A. A. Dekterev

The paper considers the aerodynamics of flow around a cubic model building. Experimental and simulation data were compared for the flow problems with different scales. Geometry parameters for the models can be varied from 0.025 to 6 m, while the range of Reynolds number for considered data is from 104 to 106. The scalability of the modeling is confirmed, which is beneficial for validity of laboratory aerodynamic experiments.

本文研究了围绕立方体模型建筑的气流动力学问题。针对不同尺度的流动问题,对实验数据和模拟数据进行了比较。模型的几何参数可在 0.025 至 6 米之间变化,而考虑数据的雷诺数范围为 104 至 106。模型的可扩展性得到了证实,这有利于实验室空气动力学实验的有效性。
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引用次数: 0
Modulation of flow meandering in the gap of a model of a peripheral subchannel of a fuel rod assembly 燃料棒组件外围子通道模型间隙中的流动蜿蜒调制
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060021
M. V. Shestakov, M. V. Tokarev

Fuel rod assemblies with tight lattice bundles are considered promising for increasing the conversion rate and heat transfer in small modular reactors. The main feature of the flow in a tight lattice rod bundle is the formation of quasi-periodic large-scale velocity oscillations in the gap between fuel rods. These oscillations enhance mixing between the subchannels and significantly increase heat transfer between the fuel rods and the coolant. The large-scale oscillations are directly related to the pitch-to-diameter (P/D) ratio of the rod bundle and the Reynolds number. In this study, we experimentally investigate the unsteady flow structure in a gap between a flat wall and three rods with a relative pitch P/D = 1.077 using time-resolved particle image velocimetry (TR-PIV) technique. The obtained TR-PIV velocity vector fields were used to analyze flow characteristics, including two- and three-dimensional mean velocity, velocity fluctuations, and Reynolds stress profiles. We also examined the influence of the Reynolds number on flow oscillations in the gap. The spatial most energy-intensive flow modes were further analyzed using the proper orthogonal decomposition (POD) method. Our results indicate the presence of several traveling waves propagating along the flow. Modulation of flow oscillations in the gap was observed. These findings are consistent with those of other researchers.

具有紧密晶格燃料棒束的燃料棒组件被认为有望提高小型模块化反应堆的转化率和传热性能。紧密晶格燃料棒束中流动的主要特征是在燃料棒之间的间隙中形成准周期性的大尺度速度振荡。这些振荡加强了子通道之间的混合,并显著增加了燃料棒与冷却剂之间的热传递。大尺度振荡与燃料棒束的节径比和雷诺数直接相关。在本研究中,我们利用时间分辨粒子图像测速仪(TR-PIV)技术,对相对间距 P/D = 1.077 的平壁与三根燃料棒之间的间隙中的不稳定流动结构进行了实验研究。获得的 TR-PIV 速度矢量场用于分析流动特性,包括二维和三维平均速度、速度波动和雷诺应力剖面。我们还研究了雷诺数对间隙中流动振荡的影响。我们使用适当的正交分解(POD)方法进一步分析了空间上能量最密集的流动模式。我们的研究结果表明,在流动过程中存在几种行波。在间隙中观察到了流动振荡的调制。这些发现与其他研究人员的研究结果一致。
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引用次数: 0
Impact of wildfire on heat and moisture transfer in a seasonally thawed layer of soil studied by numerical simulation 通过数值模拟研究野火对季节性解冻土壤层中热量和水分传递的影响
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060173
K. A. Finnikov, T. V. Ponomareva, E. I. Ponomarev, K. Yu. Litvintsev

Numerical simulation was applied to the processes of heat and moisture transfer and for ice-water phase transition in a season-thawed soil layer. Analysis was performed for consequences of natural wildfire on the soil temperature and the thawing depth as a function of water retention by soil for the condition of Siberian permafrost zone. Calculations demonstrate that the permafrost thawing depth increases due to burnouts in the top organic horizon. The quantitative indexes of natural wildfire impact depend on water retention properties of the upper organic horizon of soil.

对季节性解冻土层的热量和水分传递过程以及冰水相变过程进行了数值模拟。针对西伯利亚永久冻土带的条件,分析了自然野火对土壤温度和解冻深度的影响,以及土壤保水性的函数。计算结果表明,由于顶部有机地层被烧毁,永久冻土解冻深度增加。自然野火影响的定量指标取决于土壤上部有机层的保水特性。
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引用次数: 0
Structure of a supersonic gas-liquid jet at high liquid concentrations 高液体浓度下超音速气液射流的结构
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060069
V. M. Boiko, V. V. Lotov, A. Yu. Nesterov, S. V. Poplavski

Supersonic gas-liquid jets of a coaxial atomizer at high liquid concentrations are studied experimentally. A complex of optical techniques is used for studying the droplet sizes: visualization and particle image velocimetry, laser Doppler anemometry, and Malvern Spraytec instrument. The research shows that the velocity and concentration profiles change with flow rate growth: an extended region with small droplet velocities appears behind the bow shock wave; in this case, the concentration decreases significantly slower than that at low liquid flow rates. A small increase in the jet energy at liquid flow rates greater than 100 l/h and a noticeable increase in the droplet size testify that the gas jet capabilities for breaking up the liquid in the described regimes are exhausted.

实验研究了高液体浓度下同轴雾化器的超音速气液射流。在研究液滴大小时使用了多种光学技术:可视化和粒子图像测速仪、激光多普勒风速仪和马尔文 Spraytec 仪器。研究表明,速度和浓度剖面随流速的增长而变化:在弓形冲击波后面出现了一个液滴速度较小的扩展区域;在这种情况下,浓度的下降速度明显慢于低液体流速时的下降速度。当液体流速大于 100 升/小时时,射流能量略有增加,液滴体积明显增大,这证明在所述情况下气体射流分解液体的能力已经耗尽。
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引用次数: 0
New method of molecular modeling of liquid transport coefficients 液体传输系数分子建模新方法
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060057
V. Ya. Rudyak, E. V. Lezhnev

The paper presents a method of molecular modeling of fluid transport coefficients, which is an alternative to the method of molecular dynamics. The transport coefficients are determined using fluctuation-dissipation theorems. The dynamics of molecules is calculated stochastically, with intermolecular forces being set using the appropriate created database. A distribution function of intermolecular forces is constructed and a formula is obtained for its analytical approximation. The method effectiveness is demonstrated by the example of calculating the viscosity and thermal conductivity coefficients of liquid argon and benzene. The obtained data are compared with the data of experimental and molecular dynamic modeling and their good agreement is established. With the same modeling accuracy, the developed method is shown to be significantly more time-efficient compared to the molecular dynamics method.

本文介绍了一种流体传输系数的分子建模方法,它是分子动力学方法的一种替代方法。输运系数是利用波动-耗散定理确定的。分子动力学是随机计算的,分子间的作用力是通过创建的相应数据库设定的。构建了分子间作用力的分布函数,并获得了分子间作用力的解析近似公式。以计算液态氩和苯的粘度和导热系数为例,证明了该方法的有效性。将所获得的数据与实验数据和分子动力学建模数据进行了比较,结果表明两者具有良好的一致性。在建模精度相同的情况下,与分子动力学方法相比,所开发的方法明显更省时。
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引用次数: 0
Formulation of approximate analytical solutions for a heat transfer model for an ice layer during microwave heating 微波加热过程中冰层传热模型近似解析解的建立
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060148
V. A. Karelin, V. V. Salomatov

The research considers the microwave treatment of snow-and-ice mass comprising the stages of heating and melting. A nonlinear mathematical model for two-phase Stephan problem was developed for the case of sandwich dielectrics system. We offer approximate analytical solutions that take into account the thermophysical and electrophysical properties of dielectric layers; this approach allows parametric analysis.

摘要 该研究考虑了由加热和融化阶段组成的冰雪团块的微波处理。针对夹层电介质系统,建立了两相斯蒂芬问题的非线性数学模型。我们提供了考虑到电介质层的热物理和电物理特性的近似解析解;这种方法允许进行参数分析。
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引用次数: 0
Secondary flows in a flat diffuser and their significance for the formation of a turbulence field 平面扩散器中的二次流及其对形成湍流场的意义
IF 0.5 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2024-03-20 DOI: 10.1134/S0869864323060033
I. A. Davletshin, N. I. Mikheev, R. R Shakirov

Turbulent flows in a flat diffuser are characterized by the presence of two local maxima in the profiles of longitudinal velocity pulsations. The mechanism of the formation of a turbulent flow structure in a flat diffuser was experimentally studied. For this purpose, the parameters of the flow kinematic structure in a diffuser with an opening angle of 2.5° were measured. The profiles of velocities and turbulent characteristics of the flow in typical cross sections of the channel were obtained using the optical measurement method; based on these profiles, the secondary flows in the diffuser were identified. A physical model of the formation of the turbulent flow structure is proposed. Within the framework of this model, a high degree of turbulent pulsations far from the wall is associated with the convection of turbulence from the near-wall region into the flow core by a secondary flow in the form of an averaged spiral motion of the medium in a flat diffuser.

摘要 平面扩散器中湍流的特点是纵向速度脉动剖面存在两个局部最大值。实验研究了平面扩散器中湍流结构的形成机理。为此,测量了开口角为 2.5°的扩散器中的流动运动结构参数。利用光学测量方法获得了通道典型横截面上的流速剖面和湍流特征;根据这些剖面,确定了扩散器中的二次流。提出了湍流结构形成的物理模型。在该模型的框架内,远离壁面的高度湍流脉动与近壁区域的湍流对流有关,湍流通过平扩散器中介质平均螺旋运动形式的次级流进入流心。
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引用次数: 0
期刊
Thermophysics and Aeromechanics
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