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Evaporation characteristics of water droplets on heated surfaces with various coatings and under different wall thermal conditions 在不同壁面热条件下,不同涂层受热表面上水滴的蒸发特性
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-10-14 DOI: 10.1016/j.expthermflusci.2024.111335
Guangya Zhu, Hao Tang, Weijian Chen, Dalin Zhang, Yanjun Li, Shirui Liu
The anti-ice system is a crucial subsystem for ensuring aircraft safety. Water droplet evaporation on its surface is a frequent occurrence during flight. Investigating the characteristics of water droplet evaporation is essential for designing effective active or passive aircraft anti-ice systems. Previous research has primarily focused on the evaporation of small droplets under constant wall temperature conditions. The emergence of more electric aircraft has led to the adoption of electrical heating anti-ice systems, which typically operate under conditions of constant wall heat flux. Despite this shift, the quantitative characteristics of evaporation under different surface properties and constant wall heat flux conditions have not been thoroughly investigated. In this paper, an experimental test site was built to study the evaporation characteristics of water droplets on heating surfaces with various coatings and under different wall thermal conditions. The experimental results showed that the evaporation time for droplets on hydrophobic surfaces was longer than that on hydrophilic surfaces. The increase in evaporation time ranged from 5 to 13 times as the surface temperature was raised from 40 °C to 80 °C. Furthermore, the difference in evaporation time between small and large droplets was more pronounced under constant temperature conditions than that of constant heat flux conditions. For droplets on polished aluminum and hydrophilic surfaces, the evaporation rate was linearly related to the evaporation surface area. The findings of this study can inform future optimizations of anti-ice systems.
防冰系统是确保飞机安全的关键子系统。在飞行过程中,飞机表面经常会有水滴蒸发。研究水滴蒸发的特性对于设计有效的主动或被动飞机防冰系统至关重要。以往的研究主要集中在恒定壁温条件下的小水滴蒸发。随着更多电动飞机的出现,电加热防冰系统开始被采用,这些系统通常在恒定的壁面热通量条件下运行。尽管出现了这种转变,但对不同表面特性和恒定壁面热通量条件下蒸发的定量特征还没有进行深入研究。本文建立了一个实验测试场,研究不同涂层的加热表面在不同壁面热条件下的水滴蒸发特性。实验结果表明,水滴在疏水表面上的蒸发时间比在亲水表面上的蒸发时间长。当表面温度从 40 °C 升至 80 °C 时,蒸发时间增加了 5 至 13 倍。此外,在恒温条件下,小液滴和大液滴蒸发时间的差异比恒定热通量条件下的差异更为明显。对于抛光铝和亲水表面上的液滴,蒸发速率与蒸发表面积呈线性关系。这项研究的结果可为今后防冰系统的优化提供参考。
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引用次数: 0
Characterizing the development of gravity-driven slug flows using high-speed imaging and PIV-PLIF techniques 利用高速成像和 PIV-PLIF 技术描述重力驱动蛞蝓流的发展特征
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-10-11 DOI: 10.1016/j.expthermflusci.2024.111334
Shahriyar G. Holagh , Wael H. Ahmed
<div><div>Although developing gravity-driven slug flow frequently occurs in oil and gas, and energy systems, its development dynamics remain underexplored; this gap, in turn, has left the underlying relationships between flow evolution and transport phenomena in these applications inadequately characterized as well. The present study experimentally investigates the spatiotemporal-spectral development of gravity-driven air–water and CO<sub>2</sub>-water slug flows in a vertical 25.4 <span><math><mrow><mi>mm</mi></mrow></math></span> ID pipe. Enhanced flow visualization techniques, utilizing high-speed imaging and particle image velocimetry-planar laser induced fluorescence (PIV-PLIF), were employed to determine the behaviors of gas and liquid phases and interactions at four positions along the pipe axis. A machine vision-based algorithm was employed to extract slug unit cell characteristics and instantaneous void fraction signals, allowing for a comprehensive statistical analysis of gas phase behavior across the flow domain. A novel algorithm was also developed to preprocess raw PIV-PLIF images, facilitating phase discrimination and noise reduction before PIV cross-correlation analyses are conducted. The results showed a logarithmic growth in the lengths of Taylor bubbles, liquid slugs, and slug unit cells along the pipe, with liquid slugs constituting nearly 60 % of slug units downstream. Taylor bubble length distributions correlated well with log-normal fits, while liquid slug and unit cell lengths transitioned from log-normal patterns upstream to near-normal distributions downstream with broader and less peaked shapes. Taylor bubble velocities and appearance frequencies of the flow structures declined exponentially along the pipe, with Taylor bubble velocities showing narrower and more peaked near-normal distributions downstream. Instantaneous void fraction signals exhibited fewer, wider peaks and troughs with reduced small-amplitude oscillations downstream. The analysis of the signals indicated a complete bubbly-to-slug transition at <span><math><mrow><mi>Z</mi><mo>/</mo><mi>D</mi><mo>=</mo><mn>30</mn></mrow></math></span>. Gas-liquid phase interactions, classified as almost-zero, weak, and strong, impacted liquid phase velocity profiles and the behavior of Taylor bubbles, with minimum stable liquid slug lengths of 8–9 <span><math><mrow><mi>D</mi></mrow></math></span> and a wake length of 1.8 <span><math><mrow><mi>D</mi></mrow></math></span> observed. Empirical correlations were developed to represent the spatiotemporal-spectral aspects of flow development, with spectral parameters, particularly liquid slug frequency, identified as the most reliable indicators of the fully developed region, predicting entrance lengths of 114.0 <span><math><mrow><mi>D</mi></mrow></math></span> and 113.4 <span><math><mrow><mi>D</mi></mrow></math></span> for air–water and CO<sub>2</sub>-water, respectively. Gas density was found to strongly influence flow charact
尽管在石油、天然气和能源系统中经常出现重力驱动的蛞蝓流,但对其发展动态的探索仍然不足;而这一差距反过来又使得这些应用中的流动演变与传输现象之间的内在关系也没有得到充分描述。本研究通过实验研究了内径为 25.4 毫米的垂直管道中重力驱动的空气-水和二氧化碳-水蛞蝓流的时空谱发展。利用高速成像和粒子图像测速仪-平面激光诱导荧光(PIV-PLIF)等增强型流动可视化技术,确定了沿管道轴线四个位置的气相和液相行为及相互作用。采用基于机器视觉的算法提取蛞蝓单元特征和瞬时空隙率信号,从而对整个流域的气相行为进行全面的统计分析。此外,还开发了一种新型算法来预处理原始 PIV-PLIF 图像,以便在进行 PIV 交叉相关分析之前进行相位判别和降噪。结果表明,泰勒气泡、液体蛞蝓和蛞蝓单元的长度沿管道呈对数增长,液体蛞蝓占下游蛞蝓单元的近 60%。泰勒气泡长度分布与对数正态拟合关系良好,而液体蛞蝓和单元格长度则从上游的对数正态模式过渡到下游的接近正态分布,其形状更宽且峰值更小。泰勒气泡速度和流动结构的出现频率沿管道呈指数下降,泰勒气泡速度在下游呈现更窄、峰值更高的近似正态分布。瞬时空隙率信号显示出更少、更宽的波峰和波谷,下游的小振幅振荡减少。对这些信号的分析表明,在 Z/D=30 时,气泡完全转变为蛞蝓。气液相相互作用分为几乎为零、弱和强三种,对液相速度剖面和泰勒气泡的行为都有影响,观察到的最小稳定液滴长度为 8-9 D,唤醒长度为 1.8 D。建立的经验相关性代表了流动发展的时空-频谱方面,频谱参数,尤其是液滴频率,被确定为完全发展区域的最可靠指标,预测空气-水和二氧化碳-水的入口长度分别为 114.0 D 和 113.4 D。研究发现,气体密度对流动特性和过渡有很大影响,加速了向充分发展区的接近。
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引用次数: 0
Error analysis and improvement of water displacement method in measuring gas desorption volume from coal particles 水置换法测定煤颗粒瓦斯解吸量的误差分析与改进
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-10-10 DOI: 10.1016/j.expthermflusci.2024.111333
Xingyi Nie , Qingquan Liu , Liang Wang , Biao Lv , Yuanping Cheng
The water displacement method is widely employed in experiments to investigate the adsorption and desorption characteristics of coal gas. However, conventional desorption apparatus faces challenges in accurately quantifying gases with low desorption rates, leading to significant inaccuracies in experimental assessments of residual gas content and adsorption–desorption hysteresis. In order to solve the issue, a new desorption device was invented to carry out isothermal ultimate desorption experiments together with the conventional device under two different equilibrium pressures with coal samples of four particle sizes. The results reveal that after 100 min, the gas desorption rate gradually decreases, with the desorption percentage of the conventional device remaining relatively constant, while that of the new device continues to rise. By the end of the experiment, the conventional device measured gas residual percentages ranging from 30 % to 50 %, whereas the new device recorded percentages between 10 % and 25 %. The lower residual percentages obtained by the new device prove the effectiveness to solve the issue that the conventional devices struggle to quantify low-rate desorption gas.
When applying the conventional device, as desorption progresses, the desorption rate decreases, and the pressure within the coal sample tank increases more slowly, which results in the difficulty for the gas to reach a pressure of 71.18 Pa to overcome fluidic constraints and enter into the graduated cylinder and ultimately accumulates in the soft, large-volume silicone pipeline. In contrast, the new device, designed with its gas outlet strategically positioned above the liquid level, bypasses the constraints of liquid forces. Additionally, the modest inner diameter of the rigid tube undergoes minimal deformation under experimental conditions. Differences in liquid forces and piping allow the new device to accumulate 71 mL less gas than the conventional device. The utilization of the new device in coal gas desorption experiments effectively mitigates experimental errors stemming from low desorption rates, thereby driving advancements in the investigation of coal seam gas parameters and residual gas content.
水置换法被广泛应用于研究煤气吸附和解吸特性的实验中。然而,传统的解吸装置在准确量化解吸速率较低的气体方面面临挑战,导致残余瓦斯含量和吸附-解吸滞后的实验评估严重不准确。为了解决这个问题,我们发明了一种新的解吸装置,在两种不同的平衡压力下,用四种粒度的煤样与传统装置一起进行等温极限解吸实验。实验结果表明,100 分钟后,气体解吸率逐渐降低,传统装置的解吸率保持相对稳定,而新装置的解吸率持续上升。实验结束时,传统装置测得的气体残留率为 30% 至 50%,而新装置测得的残留率为 10% 至 25%。在使用传统装置时,随着解吸过程的进行,解吸速率降低,煤样罐内的压力增加较慢,导致气体难以达到 71.18 Pa 的压力,无法克服流体限制进入刻度量筒,最终积聚在柔软的大容量硅胶管道中。相比之下,新装置的气体出口设计在液面上方,绕过了液体压力的限制。此外,在实验条件下,内径不大的刚性管变形极小。液体作用力和管道的不同使得新装置比传统装置少积聚 71 毫升气体。在煤气解吸实验中使用新装置,可有效减少因解吸率低而产生的实验误差,从而推动煤层瓦斯参数和残余瓦斯含量研究的进步。
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引用次数: 0
Impact of piezoelectric driving waveform on performance characteristics of vibrating mesh atomizer (VMA) 压电驱动波形对振动网格雾化器(VMA)性能特征的影响
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-10-09 DOI: 10.1016/j.expthermflusci.2024.111331
Roopitha Kaimal , Jiarui Feng , Dunant Halim , Yong Ren , Voon-Loong Wong , Kean How Cheah
Vibrating mesh atomizer (VMA) is a specific type of ultrasonic atomizer known for its low power consumption and production of uniformly fine droplets. While previous research has provided a basic understanding of VMA operation, it has primarily focused on driving the piezoelectric actuator with continuous and symmetrical waveforms, such as sine and square waveforms. This study aims to experimentally investigate the impact of different driving waveforms on the ultrasonic atomization process and the associated performance characteristics. Specifically, the effects of pulse waveforms (Gauss and Lorentz pulse) were analyzed with high rates of energy deposition and asymmetrical hybrid waveforms (trapezia and absolute sine), featuring distinct negative cycles, by comparing them with conventional symmetrical waveforms (sine and square). Pulse waveforms suppress the growing stage but provide a high flux of input energy, facilitating the detachment of liquid into fine droplets, resulting in uniformly distributed droplets with VMDs of 5.84 μm and 4.71 μm for Gauss and Lorentz waveforms, respectively. Conversely, shorter negative cycles in asymmetrical hybrid waveforms reduce liquid suction into the micronozzle, leading to higher energy flux during subsequent positive cycles that promote the growing stage, producing larger droplets with VMDs of 10.82 μm and 11.86 μm for trapezia and absolute (abs) sine waveforms, respectively. Additionally, high-speed imaging reveals irregular pulsating behaviors in the atomization process when using pulse waveforms, suggesting a reciprocating-pump-like operation mechanism in VMA atomization. These new insights contribute to an improved understanding of the atomization mechanism in VMAs.
振动网格雾化器(VMA)是一种特殊类型的超声波雾化器,以其低功耗和产生均匀细小的雾滴而著称。以往的研究对 VMA 的工作原理有了基本的了解,但主要集中在用正弦波和方波等连续对称的波形驱动压电致动器。本研究旨在通过实验研究不同驱动波形对超声波雾化过程和相关性能特征的影响。具体来说,通过与传统的对称波形(正弦波和方波)进行比较,分析了高能量沉积率的脉冲波形(高斯脉冲和洛伦兹脉冲)和非对称混合波形(梯形波和绝对正弦波)的影响,它们具有明显的负循环特征。脉冲波形抑制了生长阶段,但提供了高通量的输入能量,有利于液体脱离成细小液滴,从而产生均匀分布的液滴,高斯波形和洛伦兹波形的 VMD 分别为 5.84 μm 和 4.71 μm。相反,不对称混合波形中较短的负循环减少了对微喷嘴的液体吸力,从而在随后的正循环中产生更高的能量通量,促进了生长阶段,产生更大的液滴,梯形波和绝对(abs)正弦波的 VMD 分别为 10.82 μm 和 11.86 μm。此外,在使用脉冲波形时,高速成像显示了雾化过程中的不规则脉动行为,表明在 VMA 雾化过程中存在类似往复泵的运行机制。这些新见解有助于人们更好地理解 VMA 的雾化机制。
{"title":"Impact of piezoelectric driving waveform on performance characteristics of vibrating mesh atomizer (VMA)","authors":"Roopitha Kaimal ,&nbsp;Jiarui Feng ,&nbsp;Dunant Halim ,&nbsp;Yong Ren ,&nbsp;Voon-Loong Wong ,&nbsp;Kean How Cheah","doi":"10.1016/j.expthermflusci.2024.111331","DOIUrl":"10.1016/j.expthermflusci.2024.111331","url":null,"abstract":"<div><div>Vibrating mesh atomizer (VMA) is a specific type of ultrasonic atomizer known for its low power consumption and production of uniformly fine droplets. While previous research has provided a basic understanding of VMA operation, it has primarily focused on driving the piezoelectric actuator with continuous and symmetrical waveforms, such as sine and square waveforms. This study aims to experimentally investigate the impact of different driving waveforms on the ultrasonic atomization process and the associated performance characteristics. Specifically, the effects of pulse waveforms (Gauss and Lorentz pulse) were analyzed with high rates of energy deposition and asymmetrical hybrid waveforms (trapezia and absolute sine), featuring distinct negative cycles, by comparing them with conventional symmetrical waveforms (sine and square). Pulse waveforms suppress the growing stage but provide a high flux of input energy, facilitating the detachment of liquid into fine droplets, resulting in uniformly distributed droplets with VMDs of 5.84 μm and 4.71 μm for Gauss and Lorentz waveforms, respectively. Conversely, shorter negative cycles in asymmetrical hybrid waveforms reduce liquid suction into the micronozzle, leading to higher energy flux during subsequent positive cycles that promote the growing stage, producing larger droplets with VMDs of 10.82 μm and 11.86 μm for trapezia and absolute (abs) sine waveforms, respectively. Additionally, high-speed imaging reveals irregular pulsating behaviors in the atomization process when using pulse waveforms, suggesting a reciprocating-pump-like operation mechanism in VMA atomization. These new insights contribute to an improved understanding of the atomization mechanism in VMAs.</div></div>","PeriodicalId":12294,"journal":{"name":"Experimental Thermal and Fluid Science","volume":"160 ","pages":"Article 111331"},"PeriodicalIF":2.8,"publicationDate":"2024-10-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"142422191","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Impact of a compound droplet on a solid surface: The effect of the shell on the core 复合液滴对固体表面的影响:外壳对核心的影响
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-10-05 DOI: 10.1016/j.expthermflusci.2024.111330
Yuying Du , Li Dai , Lijuan Qian , Fang Zhou , Yuechao Ma
The dynamic behavior of compound droplets impacting a solid surface was studied via experiments over κ (defined as the ratio of the compound droplet shell thickness h to the diameter D0 of compound droplet) ranging from 0 to 0.34, We ranging from 25 to 325 and Re ranging from 165.3 to 3405.2. The spreading diameter ratio, the maximum spreading dynamic contact angle and spreading speed of the core were investigated. Four modalities of the core of compound droplets were observed on the solid surface, including a) core rebound, b) no rebound, c) core splitting rebound, d) core splitting. The results revealed that the thickness of the shell, We, and the viscosity of the shell have a significant effect on the rebound and spreading processes of the core of the compound droplet. The high viscosity oil shell is conducive to its spreading. As the thickness of the oil shell increases, its cushioning effect on the water core also increases. In addition,κ=0.02254We0.503,κ=-0.336e-We121.056+0.319 and κ=0.06086e-We121.056+0.07716e-We121.70598+0.01595 were used to divide the modal boundary of the compound droplet core. Further analysis reveals the correlation between We, Re, βm and.κ,12+Weβm=8+31-cos22.78+84.57κβm3+0.955We1.05Reβm6.5.
通过实验研究了复合液滴撞击固体表面的动态行为,κ(定义为复合液滴外壳厚度 h 与复合液滴直径 D0 之比)范围为 0 至 0.34,We 范围为 25 至 325,Re 范围为 165.3 至 3405.2。研究了核心的铺展直径比、最大铺展动态接触角和铺展速度。在固体表面观察到复合液滴核心的四种模式,包括 a) 核心反弹,b) 无反弹,c) 核心分裂反弹,d) 核心分裂。结果表明,壳的厚度、We 和壳的粘度对复合液滴核心的反弹和扩散过程有显著影响。高粘度油壳有利于其扩散。随着油壳厚度的增加,其对水核的缓冲作用也会增加。此外,κ=0.02254We0.503、κ=-0.336e-We121.056+0.319 和κ=0.06086e-We121.056+0.07716e-We121.70598+0.01595 被用来划分复合液滴核心的模态边界。进一步分析发现,We、Re、βm 和.κ,12+Weβm=8+31-cos22.78+84.57κβm3+0.955We1.05Reβm6.5 之间存在相关性。
{"title":"Impact of a compound droplet on a solid surface: The effect of the shell on the core","authors":"Yuying Du ,&nbsp;Li Dai ,&nbsp;Lijuan Qian ,&nbsp;Fang Zhou ,&nbsp;Yuechao Ma","doi":"10.1016/j.expthermflusci.2024.111330","DOIUrl":"10.1016/j.expthermflusci.2024.111330","url":null,"abstract":"<div><div>The dynamic behavior of compound droplets impacting a solid surface was studied via experiments over <span><math><mi>κ</mi></math></span> (defined as the ratio of the compound droplet shell thickness <em>h</em> to the diameter <em>D<sub>0</sub></em> of compound droplet) ranging from 0 to 0.34, <em>We</em> ranging from 25 to 325 and <em>Re</em> ranging from 165.3 to 3405.2. The spreading diameter ratio, the maximum spreading dynamic contact angle and spreading speed of the core were investigated. Four modalities of the core of compound droplets were observed on the solid surface, including a) core rebound, b) no rebound, c) core splitting rebound, d) core splitting. The results revealed that the thickness of the shell, <em>We,</em> and the viscosity of the shell have a significant effect on the rebound and spreading processes of the core of the compound droplet. The high viscosity oil shell is conducive to its spreading. As the thickness of the oil shell increases, its cushioning effect on the water core also increases. In addition,<span><math><mrow><mi>κ</mi><mo>=</mo><mn>0.02254</mn><msup><mrow><mi>We</mi></mrow><mrow><mn>0.503</mn></mrow></msup><mo>,</mo><mi>κ</mi><mo>=</mo><mo>-</mo><mn>0.336</mn><msup><mrow><mi>e</mi></mrow><mfenced><mrow><mo>-</mo><mfrac><mrow><mi>We</mi></mrow><mrow><mn>121.056</mn></mrow></mfrac><mo>+</mo><mn>0.319</mn></mrow></mfenced></msup></mrow></math></span> and <span><math><mrow><mi>κ</mi><mo>=</mo><mn>0.06086</mn><msup><mrow><mi>e</mi></mrow><mrow><mo>-</mo><mfrac><mrow><mi>We</mi></mrow><mrow><mn>121.056</mn></mrow></mfrac></mrow></msup><mo>+</mo><mn>0.07716</mn><msup><mrow><mi>e</mi></mrow><mrow><mo>-</mo><mfrac><mrow><mi>We</mi></mrow><mrow><mn>121.70598</mn></mrow></mfrac></mrow></msup><mo>+</mo><mn>0.01595</mn></mrow></math></span> were used to divide the modal boundary of the compound droplet core. Further analysis reveals the correlation between <em>We</em>, <em>Re</em>, <span><math><msub><mi>β</mi><mi>m</mi></msub></math></span> and.<span><math><mrow><mi>κ</mi><mo>,</mo><mspace></mspace><mfenced><mrow><mn>12</mn><mo>+</mo><mi>W</mi><mi>e</mi></mrow></mfenced><msub><mi>β</mi><mi>m</mi></msub><mspace></mspace><mo>=</mo><mn>8</mn><mo>+</mo><mn>3</mn><mfenced><mrow><mn>1</mn><mo>-</mo><mi>c</mi><mi>o</mi><mi>s</mi><mfenced><mrow><mn>22.78</mn><mo>+</mo><mn>84.57</mn><mi>κ</mi></mrow></mfenced></mrow></mfenced><msubsup><mi>β</mi><mrow><mi>m</mi></mrow><mn>3</mn></msubsup><mo>+</mo><mn>0.955</mn><mfrac><msup><mrow><mi>We</mi></mrow><mrow><mn>1.05</mn></mrow></msup><mrow><mi>Re</mi></mrow></mfrac><msubsup><mi>β</mi><mrow><mi>m</mi></mrow><mrow><mn>6.5</mn></mrow></msubsup><mspace></mspace><mo>.</mo></mrow></math></span></div></div>","PeriodicalId":12294,"journal":{"name":"Experimental Thermal and Fluid Science","volume":"160 ","pages":"Article 111330"},"PeriodicalIF":2.8,"publicationDate":"2024-10-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"142422190","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}
引用次数: 0
Characteristics of Gas–Liquid Two-Phase flow in rectangular narrow slits with varying cross sections driven by large pressure drop 大压降驱动下不同截面矩形窄缝中的气液两相流特性
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-10-05 DOI: 10.1016/j.expthermflusci.2024.111328
Zhendong Yang, Haiyang Li, Haibo Liu, Suqi Shi, Jiaxiang Sun, Qiaoling Zhang, Guodong Li
Pressure pipelines and vessels inevitably contain some defects. Under the most unfavorable load combinations, these defects may gradually develop into through-wall cracks. High-pressure subcooled fluid leaks through these cracks, and two-phase gas–liquid flow often occurs within the cracks. In this study, natural through-wall cracks were replaced with narrow rectangular slits with varying cross sections. Experiments were conducted to investigate the variation patterns of gas–liquid two-phase leakage flow rates and pressure drops. The study focused on four types of rectangular narrow slits with varying cross sections, a width of 28 mm, a length of 80 mm, and a gap gradually ranging from 0.134 to 0.334 mm. The liquid-phase mass flow rate ranged from 150 to 700 kg/h, whereas the gas-phase mass flow rate varied from 0 to 20 kg/h. A one-dimensional homogeneous flow model was established by coupling two-phase velocity of speed calculations. This calibrated model was then used to predict pressure drops and flow parameters for gas–liquid two-phase flow in narrow rectangular slits with varying cross sections. The experimental data were analyzed to determine the two-phase leakage characteristics of different test pieces. The results show that the inlet–outlet pressure drop and flow quality are key factors affecting the two-phase leakage flow rate. The frictional pressure drop constitutes a major part of the total pressure drop along the flow path in different test pieces. Compared with the acceleration pressure drop in the expanding slit, that in the constricting slit is higher, with an increase of approximately 32 %. Among several commonly used empirical formulas for calculating two-phase viscosity, the McAdams and Dukler empirical correlations were found to be less suitable for high-velocity two-phase flows. In contrast, the Cicchitti empirical correlation provides better predictions, with a mean absolute deviation (MAD) and mean relative deviation (MRD) of no more than 8 %. The viscosity of the gas-phase medium affects the two-phase flow characteristics in narrow slits, which should be considered in practical engineering applications.
压力管道和容器不可避免地存在一些缺陷。在最不利的负载组合下,这些缺陷可能会逐渐发展成穿壁裂缝。高压过冷流体会通过这些裂缝泄漏,裂缝内往往会出现气液两相流。在本研究中,用不同横截面的窄矩形缝隙取代了天然的穿墙裂缝。实验研究了气液两相泄漏流速和压降的变化规律。研究的重点是四种截面不同的矩形窄缝,宽度为 28 毫米,长度为 80 毫米,间隙逐渐从 0.134 毫米到 0.334 毫米不等。液相质量流量为 150 至 700 千克/小时,气相质量流量为 0 至 20 千克/小时。通过耦合两相速度计算,建立了一维均质流动模型。然后,利用该校准模型来预测不同截面的窄矩形缝隙中气液两相流的压降和流动参数。通过分析实验数据,确定了不同试件的两相泄漏特性。结果表明,入口-出口压降和流动质量是影响两相泄漏流速的关键因素。摩擦压降是不同试件流道总压降的主要部分。与膨胀狭缝中的加速压降相比,收缩狭缝中的加速压降更高,大约增加了 32%。在几种常用的计算两相粘度的经验公式中,McAdams 和 Dukler 经验相关公式不太适合高速两相流。相比之下,Cicchitti 经验相关法的预测效果更好,平均绝对偏差(MAD)和平均相对偏差(MRD)均不超过 8%。气相介质的粘度会影响窄缝中的两相流特性,在实际工程应用中应加以考虑。
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引用次数: 0
Investigation on intermittent flow characteristics in horizontal pipe by visualization measurement method 用可视化测量方法研究水平管道中的间歇流动特性
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-10-02 DOI: 10.1016/j.expthermflusci.2024.111329
Bo Huang, Qiang Xu, Yeqi Cao, Haiyang Yu, Yuwen Li, Yingjie Chang, Liejin Guo
Accurate measurement and prediction of the intermittent flow characteristics in horizontal pipes is important for constructing multiphase flow models and ensuring pipe flow safety. In this paper, a quantitative image post-processing technique for intermittent flow characteristics based on gray histogram image similarity is proposed, which can realize the measurement of slug frequency. In addition, the technique also has the ability to classify a large number of images, and can quickly find the elongated bubble head, liquid film area and liquid slug area of intermittent flow. On the basis of this technique, combined with image post-processing methods such as gas–liquid interface feature analysis, a set of intermittent flow image processing technique with perfect route is formed. Based on this post-processing technique, the similarity image oscillation trajectories of plug flow and slug flow are obtained. There are differences in the similarity image oscillation trajectories of the two intermittent sub-flow patterns, and the similarity image of the plug flow has an obvious platform period and trailing rising line, which can be used as a basis for the classification of the two intermittent sub-flow patterns. A correlation for predicting the slug frequency of intermittent sub-flow patterns is developed. The accuracy of this slug frequency prediction correlation can be improved by about 10 % compared to not dividing the sub-flow patterns. When the mixture Froude number Frm is less than 5.0, the radial position of the elongated bubble head decreases linearly as the Frm increases. When the Frm is greater than 5.0, the elongated bubble head oscillates near the middle of the pipe. Prediction correlations for the radial position of the elongated bubble head and the slug velocity are established separately, and the maximum error is ± 10 %. The modified mixed Froude number is proposed, and based on this, a new prediction model for the transition from plug flow to slug flow is established.
准确测量和预测水平管道中的间歇流动特性对于构建多相流模型和确保管道流动安全非常重要。本文提出了一种基于灰度直方图图像相似性的间歇流特性定量图像后处理技术,可实现蛞蝓频率的测量。此外,该技术还具有对大量图像进行分类的能力,并能快速发现间歇流的伸长气泡头、液膜面积和液体蛞蝓面积。在此基础上,结合气液界面特征分析等图像后处理方法,形成了一套路线完善的间歇流图像处理技术。在此基础上,结合气液界面特征分析等图像后处理方法,形成了一套具有完美路线的间歇流图像处理技术。两种间歇子流形态的相似度图像振荡轨迹存在差异,塞流的相似度图像具有明显的平台周期和拖尾上升线,可作为两种间歇子流形态的分类依据。建立了预测间歇性子流型塞流频率的相关方法。与不对子流模式进行划分相比,这种蛞蝓频率预测相关性的准确性可提高约 10%。当混合物弗劳德数 Frm 小于 5.0 时,拉长气泡头的径向位置随着 Frm 的增大而线性减小。当 Frm 大于 5.0 时,拉长气泡头在管道中部附近摆动。分别建立了拉长泡头径向位置和弹头速度的预测相关性,最大误差为 ± 10%。提出了修正的混合 Froude 数,并在此基础上建立了从塞流过渡到蛞蝓流的新预测模型。
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引用次数: 0
Experimental characterization of turbulent boundary layers around a NACA 4412 wing profile NACA 4412翼型周围湍流边界层的实验特征
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-10-01 DOI: 10.1016/j.expthermflusci.2024.111327
Fermin Mallor , Carlos Sanmiguel Vila , Majid Hajipour , Ricardo Vinuesa , Philipp Schlatter , Ramis Örlü
An experimental characterization of the turbulent boundary layers developing around a NACA 4412 wing profile is carried out in the Minimum Turbulence Level (MTL) wind tunnel located at KTH Royal Institute of Technology. The campaign included collecting wall-pressure data via built-in pressure taps, capturing velocity signals in the turbulent boundary layers (TBLs) using hot-wire anemometry (HWA), and conducting direct skin-friction measurements with oil-film interferometry (OFI). The research spanned two chord-based Reynolds numbers (Rec=4×105 and 106) and four angles of attack (5°, 8°, 11° and 14°), encompassing a broad spectrum of flow conditions, from mild to strong adverse-pressure gradients (APGs), including scenarios where the TBL detaches from the wing surface. This dataset offers crucial insights into TBL behavior under varied flow conditions, particularly in the context of APGs. Key features include the quasi-independence of the pressure coefficient distributions from Reynolds number, which aids in distinguishing Reynolds-number effects from those due to APG strengths. The study also reveals changes in TBL dynamics as separation approaches, with energy shifting from the inner to the outer region and the eventual transition to a free-shear flow state post-separation. Additionally, the diagnostic scaling in the outer region under spatial-resolution effects is considered, showing further evidence for its applicability for small L+, however with inconsistent results for larger L+. The findings and database resulting from this campaign may be of special relevance for the development and validation of turbulence models, especially in the context of aeronautical applications.
在位于 KTH 皇家理工学院的最小湍流水平(MTL)风洞中,对 NACA 4412 翼型周围形成的湍流边界层进行了实验表征。活动包括通过内置压力抽头收集壁压数据,使用热线风速测量法(HWA)捕捉湍流边界层(TBL)中的速度信号,以及使用油膜干涉测量法(OFI)进行直接表皮摩擦测量。研究跨越了两个基于弦线的雷诺数(Rec=4×105 和 106)和四个攻角(5°、8°、11° 和 14°),涵盖了从轻微到强烈逆压梯度 (APG) 的各种流动条件,包括 TBL 脱离翼面的情况。该数据集为了解不同流动条件下的 TBL 行为,尤其是 APGs 背景下的 TBL 行为提供了重要依据。主要特征包括压力系数分布与雷诺数的准无关性,这有助于区分雷诺数效应和 APG 强度效应。研究还揭示了随着分离的临近 TBL 动力学的变化,能量从内部区域转移到外部区域,并最终过渡到分离后的自由剪切流动状态。此外,还考虑了空间分辨率效应下外部区域的诊断缩放,进一步证明了其对小 L+ 的适用性,但对较大 L+ 的结果并不一致。这项研究的结果和数据库可能对湍流模型的开发和验证具有特殊意义,特别是在航空应用方面。
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引用次数: 0
Experimental study of flame chemiluminescence for premixed methane based binary fuel flames 基于二元燃料的预混合甲烷火焰化学发光实验研究
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-28 DOI: 10.1016/j.expthermflusci.2024.111326
Zhengzhe Fang , Yushuai Liu , Yannis Hardalupas , A.M.K.P. Taylor
The growing requirements in using natural gas with varying compositions, biogas, syngas, and hydrogen enriched natural gas have increased the need for fuel composition and equivalence ratio sensing methods for modern gas turbine combustors. Chemiluminescence has been suggested as a promising heat release rate and equivalence ratio indicator in methane premixed flames. However, its ability in flames fuelled by the complex composition of fuels is less understood. Therefore, the main object of the present study is assessing the chemiluminescence based equivalence ratio and fuel composition sensors in binary mixtures fuelled premixed flames. The CH4 + C3H8, CH4 + CO2, and CH4 + H2 fuel mixtures are selected since they are typical compositions for the interested fuel applications. A thorough analysis of chemiluminescence characteristics including spectrum, flame patterns, chemiluminescent intensities, and intensity ratios was conducted by the measurements in a counterflow burner. The results conclude that the OH*/CH(A) chemiluminescent intensity ratio with proper removal of background emission is competent for indicating fuel composition and equivalence ratio for the examined fuel mixtures. The intensity ratio between CO2* and OH*, CH(A), and C2* can be used to monitor the proportion of C3H8, H2, and CO2 respectively in the methane-based fuel mixtures.
随着对使用不同成分的天然气、生物气、合成气和富氢天然气的要求不断提高,现代燃气轮机燃烧器对燃料成分和等效比传感方法的需求也日益增加。化学发光被认为是甲烷预混合火焰中一种很有前途的热释放率和等量比指标。然而,人们对其在燃料成分复杂的火焰中的能力了解较少。因此,本研究的主要目的是评估二元混合物燃料预混合火焰中基于化学发光的当量比和燃料成分传感器。选择 CH4 + C3H8、CH4 + CO2 和 CH4 + H2 燃料混合物是因为它们是相关燃料应用中的典型成分。通过在逆流燃烧器中进行测量,对包括光谱、火焰形态、化学发光强度和强度比在内的化学发光特性进行了全面分析。结果表明,在适当去除背景发射的情况下,OH*/CH(A) 化学发光强度比可用于指示所研究燃料混合物的燃料成分和当量比。CO2* 与 OH*、CH(A) 和 C2* 的强度比可分别用于监测甲烷基燃料混合物中 C3H8、H2 和 CO2 的比例。
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引用次数: 0
Advancements on the use of Filtered Rayleigh Scattering (FRS) with Machine learning methods for flow distortion in Aero-Engine intakes 使用滤波瑞利散射(FRS)和机器学习方法解决航空发动机进气口流动变形问题的进展
IF 2.8 2区 工程技术 Q2 ENGINEERING, MECHANICAL Pub Date : 2024-09-28 DOI: 10.1016/j.expthermflusci.2024.111325
Matteo Migliorini , Ulrich Doll , Nicholas J. Lawson , Sergey M. Melnikov , Jonas Steinbock , Michael Dues , Pavlos K. Zachos , Ingo Röhle , David G. MacManus
In-flight measurements of aerodynamic quantities are a requirement to ensure the correct scaling of Reynolds and Mach number and for the airworthiness certification of an aircraft. The ability to obtain such measurement is subject to several challenges such as instrument installation, environment, type of measurand, and spatial and temporal resolution. Given expected, more frequent use of embedded propulsion systems in the near future, the measurement technology needs to adapt for the characterization of multi-type flow distortion in complex flow, to assess the operability of air-breathing propulsion systems. To meet this increasing demand for high-fidelity experimental data, the Filtered Rayleigh Scattering (FRS) method is identified as a promising technology, as it can provide measurements of pressure, temperature and 3D velocities simultaneously, across a full Aerodynamic Interface Plane (AIP). Τhis work demonstrates the application of a novel FRS instrument, to assess the flow distortion in an S-duct diffuser, in a ground testing facility. A comparison of FRS results with Stereo-Particle Image Velocimetry (S-PIV) measurements reveals good agreement of the out of plane velocities, within 3.3 % at the AIP. Furthermore, the introduction of machine learning methods significantly accelerates the processing of the FRS data by up to 200 times, offering a substantial prospect towards real time data analysis. This study demonstrates the further development of the FRS technique, with the ultimate goal of inlet flow distortion measurements for in-flight environments.
要确保雷诺数和马赫数的正确比例以及飞机的适航认证,就必须在飞行中测量气动量。获取此类测量值的能力受到多种挑战的制约,例如仪器安装、环境、测量值类型以及空间和时间分辨率。考虑到在不久的将来嵌入式推进系统的使用会更加频繁,测量技术需要适应复杂流动中多类型流动变形的特征描述,以评估喷气推进系统的可操作性。为了满足对高保真实验数据日益增长的需求,过滤瑞利散射(FRS)方法被认为是一种很有前途的技术,因为它可以同时测量整个空气动力界面平面(AIP)上的压力、温度和三维速度。这项工作展示了新型 FRS 仪器在地面测试设施中的应用,以评估 S 型导管扩散器中的流动变形。将 FRS 结果与立体粒子图像测速仪(S-PIV)测量结果进行比较后发现,在 AIP 处,平面外速度的一致性很好,不超过 3.3%。此外,机器学习方法的引入大大加快了 FRS 数据的处理速度,最高可达 200 倍,为实时数据分析提供了广阔的前景。这项研究展示了 FRS 技术的进一步发展,其最终目标是为飞行环境测量进气道气流畸变。
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引用次数: 0
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Experimental Thermal and Fluid Science
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