相变微胶囊功能流体融化状态的数值模拟

本文用双流体模型模拟相变微胶囊(MCPCM)功能流体在大通道层流流动中的融化状态.MCPCM功能流体的入口条件和边界条件类型是影响MCPCM在管道中沿程融化率和融化速率的两个重要的决定因素.本文给出了恒壁温和恒热流两类边界条件下,不同入口条件时,MCPCM截面平均融化率和融化速率沿管道方向的变化趋势.提出了利用MCPCM的融化率与温度场的关系,通过管道截面的平均温度和截面温度场估算MCPCM截面平均融化率的思路.     

基于涡流管能量分离效应的温度分布实验研究

在入口温度、压力不变的条件下,改变冷流比,分别对不同冷流比工况下的涡流管内温度分布进行了实验测试,同时对不同冷流比工况下的实验结果进行比较,研究表明:在同一轴向端面处,温度由轴心向壁面呈现不断增大的趋势,在壁面附近处达到最大值;在同一径向位置处,温度随着轴向位置的增大不断增大,在涡流室的轴心处,温度达到最低,而在热端出口的壁面处,温度达到最大。在冷流比为0.1563时,温度沿径向呈增大趋势,而在冷流比为0.7158时,温度沿径向呈现先降低后增大的趋势;在实验研究范围内,同一测点处,温度随冷流比的增大而增大。     

高温气冷堆堆芯球床流动与温度分布均匀性研究

由于燃料球的随机分布和球床的壁面效应,球床式高温气冷堆堆芯孔隙率分布会有一定的不均匀性。深入认识壁面漏流、随机孔隙率对球床温度分布均匀性的影响对进一步提高高温气冷堆冷却剂出口温度及其安全性具有重要意义。本文采用多孔介质模型实现了对堆芯球床壁面漏流、随机孔隙率效应的数值模拟。结果表明,由于壁面漏流效应,壁面附近局部区域冷却剂最大速度会比中心高50%,对球床温度影响则不大。中心区域局部极小、极大孔隙率只对很小区域内流速和温度有影响,但温度变化幅值很小。球床中心随机孔隙率使冷却剂速度波动小于13%,对球床温度影响很小。     

HEAT TRANSFER AND PRESSURE DROP MEASUREMENTS FOR IN-TUBE CONDENSATION OF CFC-113 USING MICROFIN TUBES AND WIRE INSERTS

Accurate, repeatable heat transfer and pressure-drop measurements have been made for condensation of CFC-113 with downflow inside enhanced microfin tubes and tubes containing twisted-wire inserts. In the latter case measurements have also been made for CFC-113/air mixtures. The heat transfer rate was calculated from the coolant flow rate and temperature rise, the latter measured using a 10-junction thermopile with careful attention paid to adequate coolant mixing and isothermal immersion of the thermopile leads. The surface temperature was found from thermocouples embedded in the tube wall. One plain tube, nine microfin tubes (with different fin heights, helix angles, and number of fins), and four twisted-wire inserts (with different wire densities) were tested. Enhancement ratios (i.e., vapor-side heat transfer coefficient for the enhanced tube divided by that for a smooth tube at the same vapor-side temperature difference and vapor inlet velocity) between 1.6 and 5.6 for the microfin tubes and between 1.2 and 1.6 for the twisted-wire inserts were found, with values depending on vapor-side temperature difference, vapor inlet velocity, and air inlet mole fraction in the case of CFC-113/air mixtures. The microfin tubes showed moderate pressure-drop penalties of around 50% compared to the plain tube, while the twisted-wire inserts showed increasing pressure-drop penalty with increasing wire density.     

One-dimensional acoustic waves in retarding structures with propagation velocity tending to zero

A retarding structure that allows the effective admittance of a tube wall to increase smoothly along the tube axis is considered. The sound velocity gradually decreases along a finite segment of the tube and finally vanishes at some cross section. The time of the sound propagation along this segment is infinitely long. A wave incident on the input cross section cannot reach the other end of the tube within a finite time, and, hence, it is not reflected from it. The wave is completely absorbed, the absorption being caused by the energy accumulation in the cross section where the velocity of sound vanishes, rather than by the energy transformation to heat, as in common sound absorbers. A differential equation is obtained to describe the sound propagation in a one-dimensional waveguide with a varying cross section and varying acoustic admittance of the walls. The solutions to this equation are analyzed in the WKB approximation. An exact solution is determined for the case of some specific functions describing the variations of the cross section and admittance. Calculated results for the input admittance of the waveguide are presented. A possible similarity to the problem of shear waves in sea sediments is pointed out.     

Iterative methods for solving nonlinear problems of nuclear reactor criticality

The paper presents iterative methods for calculating the neutron flux distribution in nonlinear problems of nuclear reactor criticality. Algorithms for solving equations for variations in the neutron flux are considered. Convergence of the iterative processes is studied for two nonlinear problems in which macroscopic interaction cross sections are functionals of the spatial neutron distribution. In the first problem, the neutron flux distribution depends on the water coolant density, and in the second one, it depends on the fuel temperature. Simple relationships connecting the vapor content and the temperature with the neutron flux are used.     

Zur thermischen Wandbelastbarkeit bei toroidalem Plasmaeinschluß

In this paper a model theory is demonstrated by which it is possible to determine the load capacity of a wall including an electric arc. This theory bases on exact numerical computations of the temperature distribution inside the wall of a toroidal arc tube. It is shown and explained that the thermal load capacity increases with the radius of curvature at fixed tube radius and decreases with the tube radius at fixed radius of curvature.     

Investigating the effects of nanoparticles mean diameter on laminar mixed convection of a nanofluid through an inclined tube with circumferentially nonuniform heat flux

In this study, laminar mixed convection of a water-based nanofluid containing Al₂O₃ nanoparticles in an inclined copper tube, which is heated at the top half surface, is investigated numerically. A heat conduction mechanism through the tube wall was implemented. Three-dimensional equations using a two-phase mixture model were solved to investigate the hydrodynamic and thermal behaviors of the nanofluid over a wide range of nanoparticle volume fractions. To verify the model, the results were compared with previous works and a good agreement between the results was observed. The effect of nanoparticles diameter on the hydrodynamic and thermal parameters over a wide range of Grashof numbers is presented and discussed for a particle volume fraction and Reynolds number. It is shown that the diameter of nanoparticles affects the particle distribution in the cross section perpendicular to the tube axis, heat transfer coefficient, and shear stress.     

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用JAEA水冷包层(WCSB)模块侧壁的流量分配实验验证了SST湍流模型,建立了水冷包层模块第一壁的数值分析模型,研究了第一壁各冷却管中的流量分配情况。分析结果发现,第一壁模型入口集管中存在复杂的流动行为,冷却剂可以明显的区分为主流和逆流两大部分,其中主流进入冷却管的位置是影响流量分配的主要因素,逆流区形成了一系列次级涡流和沿管壁的环向流动。分析结果表明,在第一壁模型中,在所以条件下,各冷却剂通道中存在流量分配不均匀现象,流速最大值与最小值偏差均小于2%。     

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In order to optimize the process of plasma spheroidization of the lithium micro-powder, a 2-D model of inductively coupled thermal plasma torch is presented. The calculating domain of the electromagnetic field is extended to the air region outside the plasma discharge region and multi-physics coupling calculation was performed by using COMSOL software. The plasma electromagnetic field, temperature and velocity distributions are obtained. The physical mechanism of distributions is analyzed. The simulation found that there are two sets of symmetrical reflux vortices in the coil section of the plasma region. The velocity distribution which locates in the center of coil section and closes to the wall of confinement tube is in disorder. The plasma particles hit the wall along the radial direction. Disorderly flow may cause a rupture area along the circular tube wall. Based on the simulation results, it is proposed that in the process of inductively coupled plasma spheroidization, powder injection port can be moved down to avoid the upper reflux vortex.     

水冷包层模块局部模型流量分配数值模拟

用JAEA 水冷包层(WCSB)模块侧壁的流量分配实验验证了SST 湍流模型,建立了水冷包层模块第一壁的数值分析模型,研究了第一壁各冷却管中的流量分配情况。分析结果发现,第一壁模型入口集管中存在复杂的流动行为,冷却剂可以明显的区分为主流和逆流两大部分,其中主流进入冷却管的位置是影响流量分配的主要因素,逆流区形成了一系列次级涡流和沿管壁的环向流动。分析结果表明,在第一壁模型中,在所以条件下,各冷却剂通道中存在流量分配不均匀现象,流速最大值与最小值偏差均小于2%。     

基于COMSOL 的感应耦合等离子体炬多物理场研究

为了优化锂微粉等离子体球化的工艺,对感应耦合等离子体炬进行二维建模,将电磁场计算域扩展到等离子体放电区域之外的空气区域,利用COMSOL 软件进行多物理场模拟。得到了等离子体的电磁场、温度和速度分布,并对分布形成的物理机制进行分析。模拟发现等离子体区域线圈段存在上下两组对称的回流涡,线圈段中部靠近约束管处等离子体速度分布杂乱,有激烈的径向打壁现象,乱流预计会对约束管壁相应位置造成一条环状的破裂效果。基于模拟结果,提出在采用感应耦合等离子体球化锂微粉的工艺工程中,可以将注粉口下移,绕开上回流涡。     

带轴向温控仪的金属蒸气激光管径向温度场分析

对带轴向温控仪的金属蒸气激光放电管,建立了描述放电管径向温度场的简单数学模型.给出了由热辐射和热传导引起的径向温度变化的解析表达式,计算分析了轴向温控仪对激光管管壁温度和径向温度分布的作用机制.结果表明轴向温控仪可在一定范围内独立调节放电管管壁温度和减小激光管的径向温度梯度,可有效提高激光器运转效率和稳定性.     

基于对流传热模型的LD端面泵浦圆形激光晶体的热效应研究

通过对半导体端面泵浦棒状Nd∶YAG晶体的热效应进行了理论分析,研究了端面抽运圆形截面激光晶体内部温度场,建立了符合条件的激光晶体热模型。考虑晶体侧面与冷却液之间的对流传热,以及晶体端面与外界非绝热边界条件,从而建立更为合理的边界条件,得出更符合实际的晶体的温度分布场。研究结果表明,考虑端面的对流传热后,计算的晶体中心温度降低,而相应的热焦距稍有增加;空气传热系数增加时,晶体中心温度明显降低,热焦距显著增加,减弱了晶体热效应。     

An improved radial temperature model of a high-powered He–SrBr2 laser

When designing and modeling metal vapor and metal halide vapor lasers, the radial distribution of the gas temperature is found by solving the steady-state heat conduction equation for the internal tube at mixed boundary conditions. The volume power density is usually taken as a constant and the unknown value for the temperature of the inner wall is substituted by the measured temperature of the outer wall of the composite laser tube. In this paper, these inaccuracies are overcome. A general solution of the steady-state heat conduction problem has been suggested for an arbitrary volume power density. In order to determine the temperature of the inner wall, a complete model of the radial heat flow has been constructed. The resulting model has been applied in order to evaluate the gas temperature of a new high-powered strontium laser at different qualitative distributions of volume power density. The results have been compared with the known simple models. The presented model could be used on its own for existing and future lasers or as part of other types of theoretical or computer models.     

Impact of coolant temperature on piston wall-wetting and smoke generation in a stratified-charge DISI engine operated on E30 fuel

A late-injection strategy is typically adopted in stratified-charge direct injection spark ignition (DISI) engines to improve combustion stability for lean operation, but this may induce wall wetting on the piston surface and result in high soot emissions. E30 fuel, i.e., gasoline with 30% ethanol, is a potential alternative fuel that can offer a high Research Octane Number. However, the relatively high ethanol content increases the heat of vaporization, potentially exacerbating wall-wetting issues in DISI engines. In this study, the Refractive Index Matching (RIM) technique is used to measure fuel wall films in the piston bowl. The RIM implementation uses a novel LED illumination, integrated in the piston assembly and providing side illumination of the piston-bowl window. This RIM diagnostics in combination with high-speed imaging was used to investigate the impact of coolant temperature on the characteristics of wall wetting and combustion in an optical DISI engine fueled with E30. The experiments reveal that the smoke emissions increase drastically from 0.068 FSN to 1.14 FSN when the coolant temperature is reduced from 90 °C to 45 °C. Consistent with this finding, natural flame luminosity imaging reveals elevated soot incandescence with a reduction of the coolant temperature, indicative of pool fires. The RIM diagnostics show that a lower coolant temperature also leads to increased fuel film thickness, area, and volume, explaining the onset of pool fires and smoke.     

压力管式超临界水堆堆芯核热耦合

针对压力管式超临界水堆(PT-SCWR)新型62棒设计,其功率密度与燃料温度、冷却剂密度/温度紧密耦合,利用中子物理分析程序(WIMS-AECL)和子通道分析程序(ATHAS),对该设计堆芯进行核热耦合分析,并进行优化,结果表明该耦合方法是有效的。分析结果指出新型62棒燃料组件设计包壳最高温度和冷却剂出口温度都低于设计限值,满足设计目标;并且可以通过调整内外圈燃料富集度至5.5%和4.6%、调整燃料组件内圈棒束节圆由5.30cm到5.175cm,进行优化来获取一个均匀的温度分布;通过对比不同栅距下的慢化剂温度系数和空泡系数,得到一个最佳栅距为21cm。     

Numerical study on spinning detonations

Spinning detonations in both a circular tube and a square tube are presented in order to reveal characteristics of spinning modes by using three-dimensional simulations with a detailed chemical reaction model. The present results show a feature of a single spinning detonation which was discovered in 1926. The shock patterns in both cases are similar except the pressure trail, however, the shock wave angles and the shock wave lengths are shown to be dependent on the cross section configuration of the tube. The pitch angle, the track angle, the Mach stem angle, and the incident shock angle on the tube wall in the numerical results agree well with those in the experimental ones, and they are independent of the compositions of mixture, tube diameters, and initial pressures.     

Xe-NH (X3∑-)体系的势能面和冷碰撞动力学研究

以超冷Xe原子感应冷却NH（X³∑^-）分子实验为背景,理论研究磁场中Xe和NH的冷碰撞动力学性质.通过从头算方法得到了解析表达的Xe-NH体系势能面,并在此基础上采用量子动力学计算方法,研究了磁场条件下NH低场追索态（n=0,m_j=1）的冷碰撞塞曼弛豫截面.结果表明超冷Xe原子感应冷却NH分子可能在实验上难以实施.     

中心螺管模型线圈交流损耗计算及测试

中心螺管模型线圈选用 Nb Ti/ Cu复合超导材料 ,超导股线直径 0 .85 m m,Cu截面积与 Nb Ti截面积比为 1.38;经过 4级绞缆和成型 ,导体尺寸为 17.4 mm× 17.4 m m,中心冷却孔直径 4 .1m m。线圈用超临界氦冷却 ,流体进口温度为 3.8- 4 .2 K,压力 6 bar,每个流道流量 2 .2 g/ s。用量热法对中心螺管模型线圈进行了交流损耗测试并与计算值相比较 ,3次交流损耗电流分别是 :30 0 A/ s速度励磁和放电 ,最大电流 5 k A ,交流损耗测量值为每脉冲 78.3J;30 0 A / s速度励磁和放电 ,最大电流 7k A ,交流损耗测量值为每脉冲 14 0 .7J;4 0 0 A/ s速度励磁和放电 ,最大电流 7k A,交流损耗测量值为每脉冲14 5 .4 J;计算值分别为每脉冲 98J,1385 J,14 2 J;两者较好相符。