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Proceeding of Proceedings of the 26thNational and 4th International ISHMT-ASTFE Heat and Mass Transfer Conference December 17-20, 2021, IIT Madras, Chennai-600036, Tamil Nadu, India最新文献

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Experimental analysis of direct contact condensation during vertical injection of steam on subcooled water pool 过冷水池垂直注入蒸汽时直接接触冷凝的实验分析
Saurabh Patel, Sharey Deep Guleria, Aniket Pati, Parmod Kumar
Experiments have examined the phenomenon of direct contact condensation when steam is injected vertically into the subcooled water pool. The investigation is carried out by varying the steam mass flow rate and submergence depth of the steam injection pipe in the range of 10-50 kg/hr and 1-13 cm, respectively. The behavior of the bubble that appeared at the pipe outlet, transient heat transfer coefficient, pressure variation in the steam injection pipe, and its associated frequency have been analyzed. The images captured by high speed-camera showed different bubble shapes. The overall cycle time of bubble evolution has decreased with an increase in the mass flow rate and increased with an increase in the pipe submergence depth. The time averaged heat transfer coefficient increased with an increase in the mass flow rate and decreased with the rise of the pipe submergence depth. The pressure drop within the steam injection pipe shows the parabolic variation with an increase in the mass flow rate and is slightly influenced by the submergence depth due to changes in interfacial structures within the pipe. The peak frequency associated with the pressure has increased with an increase in the mass flow rate and decreased with an increase in the pipe submergence depth at higher mass flow rates. The FFT (Fast Fourier Transform) of interfacial area of the larger bubble at the pipe outlet shows that the first peak frequency lies between 0.5-5 Hz, and the second peak frequency lies in the range of 25-30 Hz.
实验研究了当蒸汽垂直注入过冷水池时的直接接触冷凝现象。通过在10- 50kg /hr和1- 13cm范围内改变注汽管的蒸汽质量流量和下沉深度来进行研究。分析了管道出口处气泡的行为、瞬态换热系数、注汽管内压力变化及其相关频率。高速摄像机拍摄的图像显示出不同的气泡形状。气泡演化的总循环时间随质量流量的增加而减小,随管道埋深的增加而增大。时间平均换热系数随质量流量的增加而增大,随管道埋深的增加而减小。注汽管内压降随质量流量的增加呈抛物线型变化,由于管内界面结构的变化,受浸没深度的影响较小。在高质量流量下,与压力相关的峰值频率随质量流量的增加而增加,随管道埋深的增加而降低。对管道出口较大气泡的界面面积进行FFT (Fast Fourier Transform)分析表明,第一个峰值频率在0.5 ~ 5hz之间,第二个峰值频率在25 ~ 30hz之间。
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引用次数: 2
Effect of fin location on constrained melting heat transfer of phase change material in a spherical capsule: A numerical study 翅片位置对相变材料在球形胶囊内受限熔融换热影响的数值研究
A.K. Sharma, R. Kothari, Jaykumar Joshi, V. Saxena, S. Sahu
The present work is focussed on numerical investigation of the constrained melting of phase change material (n-octadecane) in a circumferentially finned spherical capsule keeping the base and volume of the fins equal in all cases. Four different fin shapes, namely straight, trapezoidal converging, stepped, stepped inverse, located at the center of the spherical capsule are considered for the study A series of two-dimensional transient numerical simulations are carried out. Present numerical results are validated with the existing experimental results of Fan et al. [5]. Various thermal performance parameters is used for comparative analysis. Baseline comparison of fin and no fin case have also been discussed. The least melting time of PCM is 114 min for the stepped fin, while the maximum melting time is 120 min and is reported for the straight fin. The surface area to volume ratio (S/V) of fins has been calculated for every case. Irrespective of the lower S/V ratio, the melting time of inverse stepped fin is lower than straight fin because of the excellent melting performance of inverse stepped fin in weak convection region. From the results, it has been concluded that changing the shape of fin from the base case of straight fin does not change the melting time significantly for fin volume considered in the present study. This research could be used as a reference for LHTES unit fin design optimization in the industrial setting.
本文主要研究了相变材料(正十八烷)在所有情况下保持翅片的基底和体积相等的球形胶囊内的约束熔化。考虑了位于球囊中心的直线型、梯形收敛型、阶梯式、阶梯式逆型四种不同的翅片形状,进行了一系列二维瞬态数值模拟。本文的数值结果与Fan等人已有的实验结果进行了验证。采用各种热性能参数进行对比分析。并讨论了有鳍和无鳍情况下的基线比较。阶梯形翅片的最小熔化时间为114 min,直线型翅片的最大熔化时间为120 min,并计算了每种情况下翅片的表面积体积比(S/V)。尽管S/V比较低,但由于反阶翅片在弱对流区具有优异的熔化性能,其熔化时间比直翅片短。从结果可以得出结论,从直鳍的基本情况出发,改变鳍的形状不会显著改变本研究所考虑的鳍体积的融化时间。本研究可为工业环境下LHTES机组翅片优化设计提供参考。
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引用次数: 8
3D Computational Fluid Dynamics Analysis to Estimate Temperature Distribution of Spent Fuel Bundle during Dry Transfer Operation 用三维计算流体动力学分析估算干转移过程中乏燃料束的温度分布
Megha Rajguru, P. Rahatgaonkar, J. Singh, D. Datta, H. Rammohan
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引用次数: 0
Numerical simulations and analysis of flow past vertical-axis wind turbines employing the actuator line method 采用致动器线法对垂直轴风力机气流进行数值模拟与分析
S. V, Rutvik S. Solanki, V. K. Chalamalla, S. Sinha
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引用次数: 2
Analysis of Hypersonic Rarefied Reactive Flow Over RAM-C II Forebody Using hy2Foam Solver 基于hy2Foam求解器的高超声速RAM-C - II前体稀薄反应流分析
Gaurav Sharma, A. A. M.
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引用次数: 0
Towards understanding air curtain flows using RANS based numerical simulations 利用基于RANS的数值模拟来理解气幕流动
Tanmay Agrawal, N. K. Jha, V. K. Chalamalla
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引用次数: 2
Vapor Condensation of Iso-Butane over Plain Tube and 24 fpi finned tube placed horizontally 异丁烷在水平放置的平管和24fpi翅片管上的蒸汽冷凝
S. K. Sajjan, A. Dewangan
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引用次数: 0
Experimental Evaluation and Characterisation of PID Controller For Spacecraft Thermal Testing 航天器热测试PID控制器的实验评价与特性研究
Subramanya, Goutam Tanneru
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引用次数: 0
Study of a Waste Heat Recovery Cycle Using Super-Critical Carbon Dioxide as Working Fluid 超临界二氧化碳作为工质的余热回收循环研究
Lakshminarayanan Seshadri, Pramod Kumar
{"title":"Study of a Waste Heat Recovery Cycle Using Super-Critical Carbon Dioxide as Working Fluid","authors":"Lakshminarayanan Seshadri, Pramod Kumar","doi":"10.1615/ihmtc-2021.540","DOIUrl":"https://doi.org/10.1615/ihmtc-2021.540","url":null,"abstract":"","PeriodicalId":275628,"journal":{"name":"Proceeding of Proceedings of the 26thNational and 4th International ISHMT-ASTFE Heat and Mass Transfer Conference December 17-20, 2021, IIT Madras, Chennai-600036, Tamil Nadu, India","volume":"14 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"115460773","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Modelling Fast Hydrogen Deflagration in Partially Obstructed Acceleration Tube of ENACCEF and the Model Constant of Eddy Dissipation Model ENACCEF部分阻塞加速管内快速氢爆燃的建模及涡流耗散模型的模型常数
Nandan Saha, Shubham Mishra, V. Verma, J. Chattopadhyay
{"title":"Modelling Fast Hydrogen Deflagration in Partially Obstructed Acceleration Tube of ENACCEF and the Model Constant of Eddy Dissipation Model","authors":"Nandan Saha, Shubham Mishra, V. Verma, J. Chattopadhyay","doi":"10.1615/ihmtc-2021.3540","DOIUrl":"https://doi.org/10.1615/ihmtc-2021.3540","url":null,"abstract":"","PeriodicalId":275628,"journal":{"name":"Proceeding of Proceedings of the 26thNational and 4th International ISHMT-ASTFE Heat and Mass Transfer Conference December 17-20, 2021, IIT Madras, Chennai-600036, Tamil Nadu, India","volume":"18 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"116129610","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
期刊
Proceeding of Proceedings of the 26thNational and 4th International ISHMT-ASTFE Heat and Mass Transfer Conference December 17-20, 2021, IIT Madras, Chennai-600036, Tamil Nadu, India
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