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Investigation of laminar flows of a chemically active gas-dust medium in a circular tube 化学活性气体-粉尘介质在圆管内层流的研究
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060131
E. E. Peskova, V. N. Snytnikov

Laminar flows of a gas-dust medium with chemical reactions in an axisymmetric tube are studied in detail through numerical experiments. The study focuses on non-oxidative reactions of catalytic synthesis of hydrocarbons from methane. The hot walls of the tube warm up a two-phase flow of methane and catalytic nanoparticles. Heating of this flow enables endothermic conversion of methane into hydrocarbons and hydrogen. The presence of catalytic nanoparticles in the tube, which activate heterogeneous-homogeneous reactions, causes a significant deviation of the two-phase medium flow from the Poiseuille flow profile known for a single-component gas due to changes in the medium volume and viscosity. The change in the heat regime along the tube with variation in thermal conductivity of the reactive medium is investigated. Calculations are conducted for various values of the wall temperature, particle concentration, laminar flow velocity, and other parameters. It is discovered that the medium velocity and the gas component distributions in the tube volume and at the tube outlet are strongly affected by the methane activation energy on the catalytic nanoparticle surface, particle diameter, and particle concentration.

通过数值实验,详细研究了气-尘介质在轴对称管内发生化学反应的层流。研究了甲烷催化合成烃类的非氧化反应。管的热壁加热甲烷和催化纳米颗粒的两相流。对这一气流进行加热可以使甲烷吸热转化为碳氢化合物和氢气。由于介质体积和粘度的变化,催化纳米颗粒在管内的存在导致了两相介质流动与已知的单组分气体的泊泽维尔流动曲线的显著偏差。研究了反应介质导热系数随管内热态变化的规律。计算了壁面温度、颗粒浓度、层流速度等参数的不同取值。研究发现,催化纳米颗粒表面甲烷活化能、颗粒直径和颗粒浓度对介质流速和管内体积及出口气体组分分布有强烈影响。
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引用次数: 0
On the correlation of emissivity with the characteristics of simple substances 发射率与简单物质特性的关系
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060088
D. V. Kosenkov, V. V. Sagadeev

The results of correlating the emissivity of pure metals in the liquid phase with the atomic number of the element in the periodic system and the properties, which include the coefficients of thermal expansion and surface tension, are presented. The results obtained fit the Periodic law. The emissivity has a periodicity with traceable translational properties.

本文给出了纯金属在液相中的发射率与元素在周期体系中的原子序数、热膨胀系数和表面张力等性质的关系式。所得结果符合周期律。发射率具有周期性,具有可追溯的平移性质。
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引用次数: 0
Stabilization of controlled disturbances in a supersonic boundary layer by slots 超声速边界层中狭缝稳定可控扰动的研究
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060039
V. I. Lysenko, B. V. Smorodsky, A. D. Kosinov, A. A. Yatskikh, L. V. Afanasyev

A pioneering study of the influence of streamwise slots (grooves) of various depths h (corresponding to the Reynolds numbers Reh = 900 and 1300) on the stability of a supersonic (Mach number M = 2) boundary layer on a flat plate with respect to controlled disturbances of the first (vorticity) mode of instability determining the laminar-turbulent transition at M = 2 is performed. At Reynolds numbers Reh = 900 and 1300, the growth rates of three-dimensional disturbances at frequency f = 14 kHz are found to be smaller than the corresponding value for the smooth plate. Thus, it is shown that controlled disturbances of the first mode can be stabilized by streamwise aligned slots of a small depth (Reh < 1500).

对不同深度h(对应于雷诺数Reh = 900和1300)的流向槽(凹槽)对平板上超音速(马赫数M = 2)边界层稳定性的影响进行了开创性的研究,该研究涉及决定M = 2处层流-湍流过渡的第一(涡性)不稳定模式的受控扰动。在雷诺数Reh = 900和1300时,发现频率f = 14 kHz的三维扰动的增长率小于光滑板的相应值。因此,表明第一模态的可控扰动可以通过小深度的流向排列槽来稳定(Reh < 1500)。
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引用次数: 0
Pseudo turbulence in laminar and transitional regimes of an upward bubble flow in a pipe 管道中向上气泡流的层流和过渡态中的伪湍流
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060143
L. S. Timkin, R. S. Gorelik

In a bubble flow, both inherent liquid turbulence and pseudo turbulence induced by the bubbles are present. Total two-phase turbulence of the flow is determined by the interaction of these two components. The experimental values of the average wall shear stress and its pulsations obtained by eight double electrodiffusional probes located uniformly in one section along the pipe perimeter are presented. The gas phase is represented by monodisperse bubble mixtures with average diameters of 1 and 2 mm and a volumetric gas content of up to 20%. To modify the bubble Reynolds numbers, two working solutions with different viscosities were used. The superficial liquid velocity did not exceed 1 m/s. Flow regimes with deviations from the Sato hypothesis on the additivity of pseudo turbulence and inherent liquid turbulence were detected. At transitional liquid Reynolds numbers and small bubble Reynolds numbers, total two-phase turbulence is determined by pseudo turbulence, and there is no the influence of inherent liquid turbulence.

在气泡流动中,既有固有的液体湍流,也有气泡引起的伪湍流。流动的总两相湍流是由这两个组成部分的相互作用决定的。本文给出了8个双电扩散探头沿管道周长均匀放置在同一截面上所测得的平均壁剪应力及其脉动的实验值。气相由平均直径为1和2毫米的单分散气泡混合物表示,体积气体含量高达20%。为了修正气泡雷诺数,采用了两种不同粘度的工作溶液。表面液体流速不超过1m /s。在伪湍流和固有液体湍流的可加性上,检测了偏离佐藤假设的流型。在过渡液体雷诺数和小气泡雷诺数下,总两相湍流由伪湍流决定,不存在固有液体湍流的影响。
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引用次数: 0
Numerical investigation of the effect of helium injection on Görtler vortices in a compressible boundary layer 注氦对可压缩边界层Görtler涡旋影响的数值研究
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S086986432406009X
S. O. Morozov

The effect of light gas injection on the linear stage of development in a compressible boundary layer was studied. The problem is solved in the framework of linear stability theory and using the direct numerical simulation for Navier–Stokes equations. The data on the Görtler vortices growth rate and profiles are in agreement for these two methods. It was demonstrated that helium injection into a compressible boundary layer upon a concave surface can reduce the Görtler vortices growth rate.

研究了轻气注入对可压缩边界层线性发展阶段的影响。在线性稳定性理论的框架下,利用Navier-Stokes方程的直接数值模拟方法解决了这一问题。两种方法得到的Görtler涡旋增长速率和分布数据是一致的。结果表明,在凹表面的可压缩边界层中注入氦气可以降低Görtler涡旋的生长速率。
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引用次数: 0
Volumetric properties of the Li2Ca intermetallic alloy in solid and liquid states Li2Ca金属间合金在固态和液态下的体积性能
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060179
R. N. Abdullaev, R. A. Khairulin, S. V. Stankus, A. Sh. Agazhanov

The density and thermal expansion coefficients of the Li2Ca intermetallic alloy were measured in the temperature range of 284 – 906 K for the solid and liquid states by gamma-ray attenuation technique. The density jump of the Li2Ca intermetallic alloy was also measured during the solid – liquid phase transition. Data on the volumetric properties of the alloy at above room temperature were apparently obtained for the first time. A table of recommended values of the volumetric properties of the Li2Ca alloy over the entire measurement range is presented and their errors are estimated. It is confirmed that the Li – Ca melt with a calcium content of 33.33 at. % is an almost ideal solution.

用伽玛射线衰减法测定了Li2Ca金属间合金在284 ~ 906 K的固、液相温度范围内的密度和热膨胀系数。测定了Li2Ca金属间合金在固-液相变过程中的密度跃变。首次获得了室温以上合金的体积性能数据。给出了在整个测量范围内Li2Ca合金体积性能的推荐值表,并对其误差进行了估计。证实Li - Ca熔体的钙含量为33.33 at。%几乎是一个理想的解决方案。
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引用次数: 0
Dynamics of a monodispersed drop cluster rising in another immiscible liquid in a presence of surfactant 在表面活性剂存在下,单分散液滴团在另一种不混溶液体中上升的动力学
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060118
V. A. Arkhipov, A. S. Usanina

The results of an experimental study of the rising process of a cluster of monodispersed drops of isoparaffin oil in a water-glycerol solution in the presence and absence of surfactant at the interface are presented. The cluster flow for the Reynolds numbers Re = 0.01–1 was studied. The effect of initial volume concentration of drops in a cluster on the rising dynamics was evaluated. New experimental data on drag coefficient for a cluster of monodispersed drops rising in a liquid with/without surfactant at the interface were obtained.

本文介绍了一簇单分散异石蜡油滴在水-甘油溶液中,在界面存在和不存在表面活性剂的情况下上升过程的实验研究结果。研究了雷诺数Re = 0.01-1时的团簇流动。评价了簇内液滴初始体积浓度对上升动力学的影响。获得了一簇单分散液滴在有/无表面活性剂液体中上升阻力系数的新实验数据。
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引用次数: 0
Dust particle ejection from the surface of a gas-filled cavity 从充满气体的空腔表面喷出的尘埃颗粒
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060180
N. Yu. Bykov, V. V. Zakharov, I. A. Keresten, M. A. Nikitin, N. V. Obraztsov, D. N. Tonkov

The direct simulation Monte Carlo method was applied for calculation of dynamics of the gas-dust particle system within a problem of the near-nucleus gas-dust atmosphere of a comet. The study considers a gas-dynamic mechanism of dust particle ejection from the comet nucleus. This assumes existence of a dust-plugged cavity filled by sublimation products of icy content. Calculation offers the data on dust particle velocity as a function of key parameters. It is shown that the ejection velocity for a dust particle is described by one generalized parameter.

应用直接模拟蒙特卡罗方法计算了某彗星近核气体-尘埃大气中气体-尘埃粒子系统的动力学问题。该研究考虑了彗星核尘埃粒子喷射的气体动力学机制。这假定存在一个由冰含量的升华产物填充的灰尘堵塞腔。计算得到了尘粒速度随关键参数变化的数据。结果表明,抛射速度可以用一个广义参数来描述。
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引用次数: 0
Management optimization of temperature and pressure drop inside multi-core 3D integrated circuits with microchannels 微通道多核3D集成电路内温度和压降的管理优化
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060246
P. Z. Chen, Z. L. Pan

The introduction of three-dimensional integrated circuit (3D IC) technology is expected to break the limitations of Moore’s law. In response to the increasingly severe thermal management problem of multi-core 3D ICs, this paper developed a 3D IC model with double-layers and microchannels to analyze the temperature and pressure drop distribution inside the model. The effects of micro-pin fin arrangement, upper microchannel structure, coolant flow direction, and different regions on the cooling performance of the model were studied. The results show that compared to in-lined and staggered arrangement of the same proportion, the non-same proportion in-lined and staggered arrangement proposed in this paper can reduce the pressure drop by at least 31 % without increasing the maximum processor temperature. For the three structures of cuboid, cuboid (in-lined), and cylinder (in-lined), the use of cylinder (in-lined) structure in the upper microchannel can achieve better cooling performance. For counter flow and parallel flow, using counter flow can lower the maximum temperature and pressure drop; using parallel flow can reduce the average temperature and temperature gradient. In addition, compared with increasing Reynolds number of the upper microchannel, increasing Reynolds number of the bottom microchannel can achieve lower maximum temperature and pressure drop.

三维集成电路(3D IC)技术的引入有望打破摩尔定律的限制。针对多核3D集成电路日益严峻的热管理问题,本文建立了双层微通道的3D集成电路模型,分析了模型内部的温度和压降分布。研究了微针翅布置、上部微通道结构、冷却剂流动方向和不同区域对模型冷却性能的影响。结果表明,与相同比例的内联和交错排列相比,本文提出的非相同比例的内联和交错排列可以在不提高处理器最高温度的情况下将压降降低至少31%。对于长方体、长方体(直列)和圆柱(直列)三种结构,在上部微通道采用圆柱(直列)结构可以获得更好的冷却性能。对于逆流和平行流,采用逆流可以降低最高温度和压降;采用平行流可以降低平均温度和温度梯度。此外,与增加上部微通道的雷诺数相比,增加底部微通道的雷诺数可以获得更低的最高温度和压降。
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引用次数: 0
Effect of rotation on forced turbulent flow and heat transfer in a ribbed U-duct 旋转对带肋u型管道内强迫湍流流动和换热的影响
IF 0.6 4区 工程技术 Q4 ENGINEERING, AEROSPACE Pub Date : 2025-07-25 DOI: 10.1134/S0869864324060015
V. V. Ris, A. M. Levchenya, S. A. Galaev, I. A. Ignatiev

The paper presents a method and simulation results for turbulent airflow and heat transfer in a U-shaped square duct with straight sections and with two ribbed opposite sides. For a flow with Reynolds number of 6·104 and Prandtl number of 2.5, the numerical solution method was validated by comparing the simulated and experimental data on local heat and mass transfer in geometrically identical U-ducts; the ribs inclined to the duct axis by 45 and 60 deg. For one of these ducts with the rib inclination angle of 45 deg (at the same Reynolds number and Prandtl number of 0.71), the flow patterns and heat transfer were calculated for a stationary state and for a mode with rotation (with the rotation parameter values of 0.1 and 0.25). The rotation axis is perpendicular to the duct axis and parallel to the duct bending plane. The numerical data for the U-shaped duct are compared with the data for a fully developed (periodic) flow and heat transfer for a straight duct with ribbing. It is shown that for a U-duct, the effect of rotation has a positive influence on heat transfer enhancement.

本文介绍了一种u型直肋方形风管内紊流和换热的计算方法和模拟结果。对于雷诺数为6·104和普朗特数为2.5的流动,通过对几何形状相同的u型管内局部传热传质的模拟和实验数据的比较,验证了数值求解方法的有效性;肋向风管轴线倾斜45°和60°。对于其中一个肋倾角为45°的风管(在相同的雷诺数和普朗特数0.71下),计算了固定状态和旋转模式(旋转参数值为0.1和0.25)的流型和传热。旋转轴垂直于风管轴线,平行于风管弯曲面。将u形风管的数值数据与带肋的直管充分发展(周期)流动和换热的数值数据进行了比较。结果表明,对于u型管道,旋转效应对强化传热有积极的影响。
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引用次数: 0
期刊
Thermophysics and Aeromechanics
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