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Droplet breakup and evaporation in liquid-fueled detonations 液体燃料引爆中的液滴破裂和蒸发
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-26 DOI: 10.1016/j.expthermflusci.2024.111324
In liquid-fueled detonations droplets are subjected to a myriad of complex codependent physical phenomena occurring on overlapping temporal and spatial scales, resulting in rapid vaporization. The rate at which droplets vaporize is enhanced by the concurrent hydrodynamic breakup processes. This article describes experiments where small (d<125μm) droplet breakup at high Weber number O(104105) is imaged in a self-sustained liquid-fueled detonation with laser optical Mie scattering imagery. Experimental initial conditions, including the droplet size and mass distribution, are characterized and reported. Child droplet clouds generated from droplet interactions with detonation waves are observed to persist for approximately 10 mm past the detonation front and grow to the order of millimeters in width. A velocity deficit of 10% was observed for the multiphase detonations wave speed when compared to calculations for the equivalent gaseous detonations. The bulk droplet survival distances and breakup cloud morphology are compared to the predictions of relevant evaporation and breakup models. Calculations indicate that evaporation alone would result in droplet survival distances orders of magnitude longer than those observed. A droplet process whereby breakup occurs over an extended time, concurrent with evaporation, provides a phenomenological explanation. Empirical models constructed for shock-driven breakup predicted larger child droplet sizes than theoretical models based on linear stability theory, yielding survival distances and cloud shapes within the range of values seen in experiments. Droplets were however observed to persist longer than either model would predict. The discrepancy between calculations and experiment indicate that development of models tailored to droplets subject to variable acceleration are necessary to fully explain the multiphase detonation.
在以液体为燃料的爆炸中,液滴在重叠的时间和空间尺度上受到无数复杂的相互依存的物理现象的影响,导致快速汽化。同时发生的流体动力学破裂过程提高了液滴汽化的速度。本文介绍了在高韦伯数 O(104-105)的自持液体燃料爆燃中,利用激光光学米氏散射成像对小(d<125μm)液滴破裂进行成像的实验。实验的初始条件,包括液滴大小和质量分布,都得到了描述和报告。观察到液滴与爆轰波相互作用产生的子液滴云在爆轰前沿约 10 毫米处持续存在,宽度达到毫米量级。与等效气态爆轰的计算结果相比,多相爆轰波速的速度差为 10%。大量液滴的存活距离和破裂云的形态与相关蒸发和破裂模型的预测结果进行了比较。计算结果表明,仅蒸发就会导致液滴存留距离比观测到的距离长几个数量级。在蒸发的同时,液滴会在较长的时间内发生破裂,这一过程提供了一种现象学解释。与基于线性稳定性理论的理论模型相比,为冲击驱动破裂建立的经验模型预测了更大的子液滴尺寸,得出的存活距离和云形状在实验所见的数值范围内。然而,观察到的液滴持续时间比两种模型预测的都要长。计算结果和实验结果之间的差异表明,有必要开发适合于受可变加速度影响的液滴的模型,以充分解释多相起爆。
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引用次数: 0
Hypergolic fuel impacting a gelled oxidizer wall: Droplet dynamics, heat release, ignition, and flame analysis 过热燃料撞击凝胶氧化剂壁:液滴动力学、热释放、点火和火焰分析
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-24 DOI: 10.1016/j.expthermflusci.2024.111322
The combination of high-concentration solutions of hydrogen peroxide, known as High Test Peroxide (HTP), with the green fuel composed of tetramethylethylenediamine, dimethylaminoethanol, and methanol (TMEDA/DMEA/MeOH, 1:1:1 vol%), catalyzed by 1 wt% of copper chloride dihydrate, has significant potential for space hypergolic propulsion applications in terms of performance and safe operation. Besides the well-known and mature propulsion systems adopting liquid and solid propellants, gel propellants also present interesting characteristics that can be better explored to enable the creation of alternative propulsive systems. The present work employed HTP at 98 wt% with 6 wt% of fumed silica as a gelling agent to create gelled HTP (GHTP). Droplets of the green fuel impinged on a layer of GHTP placed over a glass slide, acting as a solid oxidizer, mimicked an element of a new hybrid gel/liquid hypergolic propulsion system. Data from infrared and visible light cameras enabled a detailed analysis of the dynamics of a reactive droplet impinging on a gelled oxidizer wall, as well as the heat release, ignition, and flame spread of the hypergolic GHTP/green fuel pair under open-air conditions. The heat release was observed to be distributed across concentric annular areas for both the fuel surrogate and the fuel with catalyst, before and after ignition, demonstrating a strong correlation with non-reactive droplet fluid dynamics, which was corroborated by spread diameter analysis processed from visible image data. Vapor and Ignition Delay Times (VDT and IDT) were found to be as low as 4 and 17 ms, respectively, for the highest droplet impact velocity and catalyst concentration. The reaction rate in the gas phase, considering the flame spread area, showed a dependency of both impact velocity and catalyst concentration, with the latter exhibiting a more pronounced and clear effect. The surface temperature ranges where first vaporization and ignition occurred were 60 °C 70 °C and 120 170 °C, respectively, which is close to the boiling point of methanol and the auto-ignition temperature of TMEDA. This finding, along with the chemical mechanisms in the gas phase related to the presence of a catalyst in the fuel, may be important for hypergolic ignition. The relatively low ignition temperatures and the short ignition times represent additional advantages of the present hypergolic combination for propulsion applications.
高浓度过氧化氢溶液(称为高试验过氧化氢(HTP))与由四甲基乙二胺、二甲基氨基乙醇和甲醇(TMEDA/DMEA/MeOH,1:1:1 vol%)组成的绿色燃料(1 wt%的二水氯化铜催化)的结合,在性能和安全操作方面具有空间超高压推进应用的巨大潜力。除了采用液体和固体推进剂的众所周知的成熟推进系统外,凝胶推进剂也呈现出一些有趣的特性,可以更好地加以探索,以创建替代推进系统。本研究采用含 98 wt% HTP 和 6 wt% 气相二氧化硅作为胶凝剂,制造出胶凝 HTP(GHTP)。绿色燃料滴落在玻璃载玻片上的 GHTP 层上,充当固体氧化剂,模拟了新型凝胶/液体混合双醇推进系统的一个要素。通过红外线和可见光摄像机获得的数据,可以详细分析反应液滴撞击胶状氧化剂壁的动态,以及双酚 GHTP/绿色燃料在露天条件下的热释放、点火和火焰蔓延情况。在点火前和点火后,观察到代用燃料和带催化剂燃料的热量释放都分布在同心环形区域,这表明与非反应液滴流体动力学密切相关,根据可见光图像数据处理的扩散直径分析也证实了这一点。在液滴冲击速度和催化剂浓度最高的情况下,蒸发和点火延迟时间(VDT 和 IDT)分别低至 4 毫秒和 17 毫秒。考虑到火焰扩散面积,气相中的反应速率与撞击速度和催化剂浓度有关,后者的影响更为明显和清晰。首次汽化和着火的表面温度范围分别为 60 °C ~ 70 °C 和 120 ~ 170 °C,接近甲醇的沸点和 TMEDA 的自燃温度。这一发现以及气相中与燃料中催化剂的存在有关的化学机制可能对双酚点火非常重要。相对较低的点火温度和较短的点火时间是本超醇类组合在推进应用方面的额外优势。
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引用次数: 0
Visualization study on the dynamic behavior of shear thinning droplets impacting superhydrophobic spheres 剪切稀化液滴撞击超疏水球体动态行为的可视化研究
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-21 DOI: 10.1016/j.expthermflusci.2024.111318
The surface and droplet characteristics significantly affect the dynamic of droplet impact on solid surfaces. In present work, a platform is utilized to experimentally study the dynamic behavior of shear thinning fluid droplets impacting superhydrophobic spheres, where the effects of different concentrations, Weber numbers (We), particle size ratios on droplets impact are studied. The results showed that on the superhydrophobic sphere, as the shear thinning droplet concentration increases, the diffusion diameter increases, and the contact time decreases. For the same curvature, the contact time between the droplet and the sphere decreases with the increase of the We. When the We reaches 75 or above, the contact time remains constant with an increase in the We. For various curvature conditions, the contact time increases as the curvature increasing. When the diameter ratio of the sphere to the droplet is D6, the maximum diffusion coefficient remains almost constant. However, when D<6, the maximum diffusion dimensionless diameter significantly increases as the particle size ratio decreases. More importantly, a theoretical model considering gravity effect is presented to predict the maximum dimensionless diameter of shear thinning droplets on superhydrophobic spheres according to energy conservation. The predicted results are rationally agreement with experiments with the deviation within ±10 %.
表面和液滴特性对液滴撞击固体表面的动态效果有很大影响。本研究利用实验平台研究了剪切稀化液滴撞击超疏水球体的动态行为,研究了不同浓度、韦伯数(We)、粒径比对液滴撞击的影响。结果表明,在超疏水球上,随着剪切稀化液滴浓度的增加,扩散直径增大,接触时间缩短。在曲率相同的情况下,液滴与球面的接触时间随 We 值的增加而减少。当 We 值达到 75 或以上时,接触时间随 We 值的增加而保持不变。在各种曲率条件下,接触时间随着曲率的增加而增加。当球体与液滴的直径比 D∗≥6 时,最大扩散系数几乎保持不变。然而,当 D∗<6 时,随着粒径比的减小,最大扩散无量纲直径明显增大。更重要的是,根据能量守恒,提出了一个考虑重力效应的理论模型来预测超疏水球上剪切稀化液滴的最大无量纲直径。预测结果与实验结果吻合,偏差在±10%以内。
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引用次数: 0
A study on the wake structure of an ascending submersible with silk flexible appendages using continuous wavelet transform and dynamic mode decomposition 利用连续小波变换和动态模式分解研究带有丝质柔性附肢的上升式潜水器的尾流结构
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-21 DOI: 10.1016/j.expthermflusci.2024.111323
This study proposed a new method for installing silk flexible appendages on the surface of the submersible to modify the wake structure of ascending submersibles, and explored a method of drag reduction of ascending submersible. A comparative analysis of the flow structure of submersibles with varying appendage lengths was conducted to understand the disturbance characteristics of the wake flow structure of submersible, and the high-speed particle image velocimetry (PIV) measurement experiment was conducted at a Reynolds number of 6456. Analysis of the time-averaged flow field showed that the flexible appendages could disrupt the two large-scale vortices in the wake of the submersibles during the sailing process, but this ability diminished with increasing appendage length. Furthermore, continuous wavelet transform (CWT) and dynamic mode decomposition (DMD) were used to analyze the mechanism behind this phenomenon. The analysis results showed that flexible appendages based on CWT had an inhibitory effect on large-scale flow, and this effect gradually decreased with increasing appendage length. The results indicate that the flexible appendages can disrupt the wake vortex structure, reduce vortex energy, and facilitate the transition from large-scale vortex to small-scale vortex. Additionally, excessive disturbance is generated in the wake region when the flexible appendage is too long, hindering the shedding of small-scale vortices and resulting in an increase.
本研究提出了一种在潜水器表面安装丝质柔性附肢以改变上升式潜水器尾流结构的新方法,并探索了一种降低上升式潜水器阻力的方法。为了解潜水器尾流结构的扰动特性,对不同附肢长度潜水器的流动结构进行了对比分析,并在雷诺数为 6456 的条件下进行了高速粒子图像测速(PIV)测量实验。对时间平均流场的分析表明,在潜水器航行过程中,柔性附肢能扰乱尾流中的两个大尺度漩涡,但这种能力随着附肢长度的增加而减弱。此外,还利用连续小波变换(CWT)和动模分解(DMD)分析了这一现象背后的机理。分析结果表明,基于 CWT 的柔性附属物对大规模流动具有抑制作用,并且这种作用随着附属物长度的增加而逐渐减弱。结果表明,柔性附属物可以破坏尾流涡旋结构,降低涡旋能量,促进大尺度涡旋向小尺度涡旋的过渡。此外,当柔性附属物过长时,会在尾流区域产生过多扰动,阻碍小尺度涡旋的脱落,导致涡旋增加。
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引用次数: 0
Contactless thermal diffusivity characterization of second order magnetocaloric materials under magnetic field using modulated photo-thermal radiometry method with very low power probe beam 利用调制光热辐射测量法和极低功率探针光束,对磁场下的二阶磁致性材料进行非接触式热扩散表征
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-18 DOI: 10.1016/j.expthermflusci.2024.111321

The thermal diffusivity of magnetocaloric materials has a transition point at a given temperature that depends on the intensity of the applied magnetic field. Consequently, a fine temperature resolution on the material sample is needed to obtain an accurate determination of the thermal diffusivity variation with temperature. The coupling between the external and the internal fields has to be carefully mastered since the pertinent operating condition is fixed by the actual internal field which is not directly measurable and may be heavily affected by any element in contact with the sample. Therefore, contactless methods such as Photo-Thermal Radiometry (PTR) are privileged. The latter is based on a radiative excitation of the front face of a thin sample and the detection of the thermal effect on the opposite face. However, the powerful radiative source may significantly increase the sample temperature which is not suitable for caloric materials. In this work, a low power modulated PTR method is proposed to characterize second order magnetocaloric materials under magnetic field. It was compared to high energy thermo-flash PTR and validated on common materials such as steel and stainless steel, and then applied to gadolinium which is the reference magnetocaloric material for magnetic refrigeration and heat pumping study. The thermal diffusivity of gadolinium samples is measured in the 285.1 K to 305.1  K temperature range, including the magnetic transition temperature without and under an external magnetic flux density of 0.5 T in the 13 mm air gap of the permanent magnet magnetic circuit. The low power probe beam ensures a temperature stability with a negligible sample temperature fluctuation less than 0.05 K on the incident sample surface and less than 0.03 K on the measurement surface. The experimental results without magnetic field align with those using other methods including the magnetic transition temperatures determination. This low-power optical method proved its efficiency to characterize highly temperature dependent materials such as magnetocaloric materials sensitive to magnetic field. The data obtained partly fills the lack of information in the literature on excited gadolinium.

磁致性材料的热扩散率在给定温度下有一个过渡点,该点取决于外加磁场的强度。因此,要准确测定热扩散率随温度的变化,需要对材料样品进行精细的温度分辨。外部磁场和内部磁场之间的耦合必须仔细掌握,因为相关的工作条件是由实际内部磁场决定的,而实际内部磁场是无法直接测量的,并且可能会受到与样品接触的任何元素的严重影响。因此,光热辐射测量法(PTR)等非接触式方法就显得尤为重要。后者基于对薄样品正面的辐射激发和对反面热效应的检测。然而,强大的辐射源可能会显著提高样品的温度,这并不适合热量材料。本研究提出了一种低功率调制 PTR 方法,用于表征磁场下的二阶磁致热材料。该方法与高能量热闪烁 PTR 进行了比较,并在钢和不锈钢等常见材料上进行了验证,然后应用于磁制冷和热泵研究的参考磁致性材料钆。钆样品的热扩散率是在 285.1 K 至 305.1 K 的温度范围内测量的,包括永磁磁路 13 mm 气隙中无外部磁通密度 0.5 T 和外部磁通密度 0.5 T 时的磁转变温度。低功率探针光束确保了温度稳定性,入射样品表面的样品温度波动小于 0.05 K,测量表面的样品温度波动小于 0.03 K。无磁场实验结果与使用其他方法(包括磁转变温度测定)得出的结果一致。这种低功率光学方法证明了它在表征高温度依赖性材料(如对磁场敏感的磁致性材料)方面的效率。所获得的数据部分填补了激发钆文献资料的空白。
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引用次数: 0
Measurement of local Nusselt number and local recovery factor for impinging multiple compressible jets 测量撞击多可压缩射流的局部努塞尔特数和局部恢复因子
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-18 DOI: 10.1016/j.expthermflusci.2024.111320
In the present study the appropriate reference temperature is identified for the compressible impinging jet. Using the measured reference temperature, local recovery factor is calculated. The steady state thin metal foil technique is used for the measurement of target plate temperature. In this study, the effect of Mach number (Ma) at a constant Reynolds number (Re) and the combined effect of Mach number and Reynolds number on the heat transfer rate are investigated. For both the cases, jet-to-plate distance is varied from z/d = 5 to 12. For the first case (effect of Mach number at a constant Re = 20,000), Ma is varied from 0.15 to 0.85. In the second case (combined effect of Mach number and Reynolds number), Ma is varied from 0.2 to 0.78 and the corresponding Re variation is 7200 to 29,000. At a constant Reynolds number, the heat transfer coefficient increases with the increase in the Mach number. For a given Mach number and Reynolds number, the heat transfer rate decreases with the increase in the jet-to-plate distance. The recovery factor remains unaffected by the Mach number and jet-to-plate distance in the case of the concurrent variation of the Mach number and Reynolds number.
本研究为可压缩撞击射流确定了适当的参考温度。利用测得的参考温度计算局部恢复系数。稳态薄金属箔技术用于测量目标板温度。在这项研究中,研究了马赫数(Ma)在雷诺数(Re)恒定时的影响,以及马赫数和雷诺数对传热速率的综合影响。在这两种情况下,射流到板的距离在 z/d = 5 到 12 之间变化。在第一种情况下(马赫数在恒定 Re = 20,000 条件下的影响),Ma 的变化范围为 0.15 至 0.85。在第二种情况下(马赫数和雷诺数的综合影响),Ma 的变化范围为 0.2 至 0.78,相应的 Re 变化范围为 7200 至 29000。在雷诺数不变的情况下,传热系数随着马赫数的增加而增加。在给定的马赫数和雷诺数下,热传导率随着射流到平板距离的增加而降低。在马赫数和雷诺数同时变化的情况下,恢复系数不受马赫数和喷射板间距的影响。
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引用次数: 0
An experimental acoustofluidic system for analyzing boundary-driven acoustic streaming generated by flat and curved walls 用于分析平墙和曲墙产生的边界驱动声流的声流体实验系统
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-14 DOI: 10.1016/j.expthermflusci.2024.111319

While boundary-driven acoustic streaming in fluids surrounded by flat walls has been extensively studied in the literature, theoretical studies on boundary-driven acoustic streaming generated by curved walls have recently emerged. This paper aims to present a quantitative analysis of acoustic streaming fields driven by forces induced by both flat and curved walls. A semi-circular channel made of stainless steel was designed to serve as a model channel with both flat and curved boundaries. A multi-layered glass-steel-glass device, actuated by a piezoelectric transducer, was assembled for experimental characterization of boundary-driven acoustic streaming in such scenarios. First, the various standing acoustic modes in the semi-circular channel were measured through the acoustophoretic patterning of 20 µm polystyrene particles. Next, the acoustic radiation force fields and boundary-driven acoustic streaming patterns under various resonant acoustic modes were characterized through micro-particle-image-velocimetry measurements of the motion of 20 µm and 1 µm polystyrene particles, respectively. Finally, the experimental results were explained using efficient finite element simulations of acoustofluidics and acoustophoresis in a semi-circular reduced-fluid model, with a focus on analyzing the streaming velocities driven by the flat and curved walls. Both experimental and numerical results demonstrated that the ratio of streaming velocities induced by the flat wall and the curved wall in this semi-circular channel depends on the resonant acoustic modes. This research highlights the diverse boundary-driven acoustic streaming patterns that arise in irregular channels and provides a theoretical foundation for choosing strategies for shape optimization to suppress acoustic streaming in acoustofluidic devices.

虽然文献中对被平壁包围的流体中的边界驱动声流进行了广泛的研究,但最近出现了对弯曲壁产生的边界驱动声流的理论研究。本文旨在对由平壁和曲壁引起的力驱动的声流场进行定量分析。本文设计了一个由不锈钢制成的半圆形通道,作为具有平面和曲面边界的模型通道。我们组装了一个由压电换能器驱动的多层玻璃-钢-玻璃装置,用于在这种情况下对边界驱动的声流进行实验表征。首先,通过对 20 微米的聚苯乙烯颗粒进行声速图案化,测量了半圆形通道中的各种驻留声学模式。接着,通过对 20 微米和 1 微米聚苯乙烯颗粒运动的微观粒子成像-测速测量,分别描述了各种共振声学模式下的声辐射力场和边界驱动声流模式。最后,在一个半圆形还原流体模型中,利用声流体学和声oresis 的高效有限元模拟解释了实验结果,重点分析了由平面和曲面壁驱动的流速度。实验和数值结果表明,在这个半圆形通道中,平壁和曲壁诱导的流速之比取决于共振声学模式。这项研究强调了不规则通道中出现的多种边界驱动声流模式,并为选择形状优化策略以抑制声流体设备中的声流提供了理论基础。
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引用次数: 0
Free surface vortex and associated air entrainment during liquid drainage using two outlets 使用两个出口进行液体排放时的自由表面涡流和相关空气夹带
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-13 DOI: 10.1016/j.expthermflusci.2024.111314

Plughole vortex dynamics and the corresponding air entrainment is of paramount importance in various process industries. The present study experimentally investigates plughole vortex induced air entrainment during the drainage of water through two closely spaced outlets from a tank. The discharge from the two outlet tubes has been modulated and the different stages of air entrainment including formation of air lamella, periodic slug bubble pinch-off, and transition into the stable annular flow are observed. The transition between the slug bubble pinch-off and the stable annular flow has been modelled by balancing the local dynamic pressure of the fluid and the Laplacian pressure jump across the gas-liquid interface. The balance yields the ratio of critical height, Hc and radius of the stable air neck, rm as Hc/rm30.68Bo-0.904fD,re-0.210, with the Bond number, Bo=ΔρgD2/σ and the geometric parameter, fD,re=1-2reD2.

在各种加工工业中,堵孔涡流动力学和相应的空气夹带至关重要。本研究通过实验研究了水箱中两个间隔较近的出水口排水时塞孔涡流引起的空气夹带。对两个出水管的排水量进行了调制,并观察了空气夹带的不同阶段,包括空气薄片的形成、周期性蛞蝓气泡夹断以及向稳定环形流的过渡。通过平衡流体的局部动态压力和气液界面上的拉普拉斯压力跃迁,模拟了蛞蝓气泡挤压和稳定环形流之间的过渡。平衡得出临界高度 Hc 与稳定气颈半径 rm 之比为 Hc/rm≈30.68Bo-0.904fD,re-0.210,其中邦德数 Bo=ΔρgD2/σ 和几何参数 fD,re=1-2reD2。
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引用次数: 0
SAMPO-P: A prototypical scale low-temperature experiment on two-layer melt pool heat transfer in LWR lower head SAMPO-P:关于低浓铀浓缩反应堆下封头两层熔池传热的原型规模低温实验
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-12 DOI: 10.1016/j.expthermflusci.2024.111303
To better understand the thermal behavior of a two-layer melt pool with a high Rayleigh number—a pattern observed in the RASPLAV study, which indicates a significant risk to pressure vessel integrity and the success of in-vessel retention (IVR) strategies—this paper reports experimental findings from a 2D, full-scale (1:1 ratio) prototypical stratified melt pool (SAMPO-P). A series of experimental tests were carried out with varying heating powers and top layer heights, achieving a Rayleigh number of 3.77×1015, comparable to that found in light water reactors (LWR). Water was used to simulate the bottom layer, while n-octanol represented the top layer. Internal decay heat was modeled in the bottom layer using electric heating rods. After analyzing the main heat transfer parameters from the experiment, this paper derived several useful heat transfer correlations. The normalized temperature and heat flux distributions remained consistent across different power levels, and the normalized heat flux in the bottom layer aligned well with existing experimental correlations. In the bottom layer, the downward heat transfer coefficient was lower compared to other single-layer correlations, likely due to increased upward heat transfer.
为了更好地了解高雷利数双层熔池的热行为--RASPLAV 研究中观察到的模式表明压力容器的完整性和舱内滞留(IVR)策略的成功面临重大风险--本文报告了二维全尺寸(1:1 比例)原型分层熔池(SAMPO-P)的实验结果。在不同的加热功率和顶层高度下进行了一系列实验测试,雷利数达到 3.77×1015,与轻水反应堆(LWR)中的雷利数相当。水被用来模拟底层,而正辛醇则代表顶层。在底层使用电热棒模拟内部衰变热。在分析了实验中的主要传热参数后,本文得出了几种有用的传热相关性。不同功率水平下的归一化温度和热通量分布保持一致,底层的归一化热通量与现有的实验相关性非常吻合。与其他单层相关性相比,底层的向下传热系数较低,这可能是由于向上传热增加所致。
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引用次数: 0
Twelfth Mediterranean Combustion Symposium 第十二届地中海燃烧研讨会
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-11 DOI: 10.1016/j.expthermflusci.2024.111317
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Experimental Thermal and Fluid Science
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