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Unusual coastal ocean cooling in the northern South China Sea by a katabatic cold jet associated with Typhoon Mujigea(2015) 被引量:2
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作者 Yuxin Shi Lingling Xie +3 位作者 Quanan Zheng Shuwen Zhang Mingming Li Junyi Li 《Acta Oceanologica Sinica》 SCIE CAS CSCD 2019年第5期62-75,共14页
This study deals with a unusual cooling event after Typhoon Mujigea passed over the northern South China Sea(SCS) in October 2015. We analyze the satellite sea surface temperature(SST) time series from October 3 to 18... This study deals with a unusual cooling event after Typhoon Mujigea passed over the northern South China Sea(SCS) in October 2015. We analyze the satellite sea surface temperature(SST) time series from October 3 to 18,2015 and find that the cooling process in the coastal ocean had two different stages. The first stage occurred immediately after typhoon passage on October 3, and reached a maximum SST drop of –2℃ on October 7 as the usual cold wake after typhoon. The second stage or the unusual extended cooling event occurred after 7d of the typhoon passage, and lasted for 5d from October 10 to 15. The maximum SST cooling was –4℃ and occurred after 12d of typhoon passage. The mechanism analysis results indicate that after landing and moving northwestward to the Yunnan-Guizhou Plateau(YGP), Typhoon Mujigea(2015) met the westerly wind front on October 5. The lowpressure and positive-vorticity disturbances to the front triggered meridional air flow and low-pressure trough,thus induced a katabatic cold jet downward from the Qinghai-Tibet Plateau(QTP) passing through the YGP to the northwestern SCS. The second cooling reached the maximum SST drop 4d later after the maximum air temperature drop of –9℃ on October 11. The simultaneous air temperature and SST observations at three coastal stations reveal that it is this katabatic cold jet intrusion to lead the unusual SST cooling event. 展开更多
关键词 TYPHOON Mujigea(2015) second-round coolING katabatic COLD jet South China Sea WESTERLY wind front
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Experimental and Numerical Investigations of the Double-Jet Film Cooling Technology 被引量:1
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作者 K. Kusterer A. Elyas +3 位作者 D. Bohn T. Sugimoto R. Tanaka M. Kazari 《Journal of Energy and Power Engineering》 2010年第9期16-25,共10页
The Double-Jet Film-Cooling (DJFC) technology is invented by the authors and comprises a significant enhancement of the adiabatic film-cooling effectiveness due to the formation of anti-kidney vortices. The DJFC tec... The Double-Jet Film-Cooling (DJFC) technology is invented by the authors and comprises a significant enhancement of the adiabatic film-cooling effectiveness due to the formation of anti-kidney vortices. The DJFC technology places a second ejection hole with compound angle in a double-hole arrangement downstream the first hole. The second hole creates a second jet with another dominating vortex rotating in opposite direction to the first one and then combines both jets to one jet. The basic applicability and function of the DJFC technology has been proven by the numerical studies and testing in a test rig. The comparison of the experimental results of the adiabatic film cooling effectiveness to the numerical results for the same blowing ratio (M=(pc)c/(pc)h) shows qualitatively similar distributions. However, the experimental results show enhanced mixing-out of the cooling air and, thus, the experimental values of the adiabatic film cooling effectiveness are lower compared to the numerical values. 展开更多
关键词 Gas turbine film-cooling cooling jets film-cooling effectiveness
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Experimental Study of Jet Nanofluids Impingement System for Cooling Computer Processing Unit 被引量:1
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作者 Paisarn Naphon Somchai Wongwises 《Journal of Electronics Cooling and Thermal Control》 2011年第3期38-44,共7页
An experimental investigation of the jet nanofluids impingement heat transfer characteristics of mini-channel heat sink for cooling computer processing unit of personal computer is performed. The experiments are teste... An experimental investigation of the jet nanofluids impingement heat transfer characteristics of mini-channel heat sink for cooling computer processing unit of personal computer is performed. The experiments are tested under the real personal computer operating conditions: no load and full load conditions. The experiments are performed for the following ranges of the parameters: coolant flow rate varies from 0.008 to 0.020 kg/s, the nozzle diameter is set to 1.00, 1.40, 1.80 mm, the distance nozzle-to-fins tip is 2.00 mm, the channel width of the mini-channel heat sink is 1.00 mm. The nanofluids with suspending of TiO2 particles in base fluid are used as a working fluids. It was observed that the average CPU temperatures obtained from the jet nanofluids impingement cooling system are 3.0%, 6.25% lower than those from the jet liquid impingement and from the conventional liquid cooling systems, respectively. However, this cooling system requires higher energy consumption. 展开更多
关键词 jet IMPINGEMENT Nanofluids coolING coolING CPU Mini-Rectangular Fin Heat SINK
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Best Determined Position of Vents Based on Jet Cooling Model
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作者 Na Huang Yuhan Sun Xiangjie Wu 《Journal of Mechanical Engineering Research》 2020年第1期25-29,共5页
In some data centers,cold air is required to act on the cabinet to achieve cooling requirements,and the mixing of cold air and hot air reduces the utilization efficiency of cold air.In order to solve this problem,a je... In some data centers,cold air is required to act on the cabinet to achieve cooling requirements,and the mixing of cold air and hot air reduces the utilization efficiency of cold air.In order to solve this problem,a jet cooling model is established to solve the optimal position of the outlet through the movement of cold air. 展开更多
关键词 Optimal Scheme jet cooling Model Fourier law Thermal Conductivity
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On the Method of Air Jet Cooling in Green Manufacturing
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作者 REN Jia long East China Shipbuiling Institute, Zhenjiang 212003, P.R.China 《International Journal of Plant Engineering and Management》 2001年第4期186-192,共7页
Green cooling is an important technology in green manufacturing. In the way of jetting, cooling airflo-w in used in the experiments of metal material cutting, by comparison of the changes of some technological factors... Green cooling is an important technology in green manufacturing. In the way of jetting, cooling airflo-w in used in the experiments of metal material cutting, by comparison of the changes of some technological factors, such as cutting heat, surface finish, in the process of jet cooling, pour cooling and natural cooling, we can draiv the conclusion that air jet cooling has a better cooling effect and green function. It can be 'widely used in both traditional and automatic green manufacturing. 展开更多
关键词 TURNING jet cooling green manufacturing air cooling
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Experimental Investigation of the Cooling Capacity of Gaseous Carbon Dioxide in Free Jet Expansion for Use in Portable Air-Cooling Systems
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作者 Chady Al Sayed Ludwig Vinches Stéphane Hallé 《Open Journal of Applied Sciences》 2018年第2期62-72,共11页
This paper investigates the possibility of using the free expansion of gaseous CO2 in portable air-cooling systems. The cooling capacity of the gaseous CO2 free jet expansion was calculated using three different appro... This paper investigates the possibility of using the free expansion of gaseous CO2 in portable air-cooling systems. The cooling capacity of the gaseous CO2 free jet expansion was calculated using three different approaches and the results showed that the simplified calculations would give approximated cooling values with an 11.6% maximum error. The mass flow rate, upstream pressure and cooling capacity of the gaseous CO2 decreased with time. A maximum 48.5 watts of cooling was recorded at minute 4 and a minimum value of 10.4 watts at the end of the test. The drop in cooling capacity is due to the evaporation of the liquid CO2 inside the small cylinder which cools the two-phase CO2 mixture and causes a pressure drop (from 6 MPa to 2.97 MPa), which also affects the mass flow rate of gaseous CO2 exiting the orifice (from 0.56 g/s to 0.24 g/s). If this cooling technique is to be considered in portable compact-cooling systems, the mass, pressure and cooling capacity drop with time must be solved. One of the solutions could be to cover the cylinder with a heating coat to compensate for the heat absorbed by the evaporation of the liquid CO2. 展开更多
关键词 Gaseous CO2 Free jet EXPANSION coolING Capacity Compact Air-cooling Technique
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LES of film cooling for different jet fluids
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作者 P. Renze W. Schroeder M. Meinke 《航空动力学报》 EI CAS CSCD 北大核心 2007年第4期521-530,共10页
关键词 航空推进系统 仿真 横向流动式喷气 密度比 速率 冷却效率 薄雾冷却
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射流冲击-再生通道复合冷却性能的实验研究
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作者 李勇 张劲 +4 位作者 周棋润 张迎春 杨森杰 马素霞 谢公南 《航空动力学报》 北大核心 2026年第2期35-44,共10页
为了验证射流冲击-再生通道复合冷却技术的可行性,采用稳态液晶技术来实验测量环境空气仅初始横流、仅射流和射流-初始横流复合冷却方式下的努塞尔数。实验结果表明:仅射流冷却和射流-初始横流复合冷却相比于仅初始横流冷却的传热效果... 为了验证射流冲击-再生通道复合冷却技术的可行性,采用稳态液晶技术来实验测量环境空气仅初始横流、仅射流和射流-初始横流复合冷却方式下的努塞尔数。实验结果表明:仅射流冷却和射流-初始横流复合冷却相比于仅初始横流冷却的传热效果分别提高了207.55%~370.24%和428.35%~545.35%,并且所有流量条件下射流-初始横流复合冷却的传热性能均优于仅射流冷却的情况。射流孔数量、射流流量和初始横流流量三者之间存在最佳优化关系可使得传热性能最大化:射流可大幅提升靶面传热性能但随着流量的增加提升幅度减弱,并且射流孔数量的增加可提高靶面温度分布均匀性;射流触及靶面且动量适宜时初始横流可进一步有效提升努塞尔数;流量过小导致射流无法触及靶面时初始横流和射流的共同扰动作用也可提高传热性能。 展开更多
关键词 超燃冲压发动机 再生冷却 射流冲击 初始横流 努塞尔数
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相变材料结合空气射流混合式电池热管理系统性能研究
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作者 袁长顺 赵彦琦 丁玉龙 《储能科学与技术》 北大核心 2026年第3期838-847,共10页
相变材料(phase change material,PCM)冷却是电池热管理中常用的方式,能够在维持电池模组温度场均匀性的同时保障系统安全。然而,由于锂离子电池正负极材料本身在结构和热特性上的差异,其两端往往存在明显的温度不均,仅依靠PCM冷却难以... 相变材料(phase change material,PCM)冷却是电池热管理中常用的方式,能够在维持电池模组温度场均匀性的同时保障系统安全。然而,由于锂离子电池正负极材料本身在结构和热特性上的差异,其两端往往存在明显的温度不均,仅依靠PCM冷却难以有效消除此类局部热隐患。为此,本研究提出一种结合PCM冷却与空气射流风冷的混合热管理策略。该方案在电池正极一侧施加空气射流强化冷却,同时将整个模组包覆于石蜡中,通过调节射流阵列布置与空气质量流量,系统分析其在车辆能耗与续航里程测试中对电池温度场的影响。研究结果表明,在控制空气质量流量的条件下,在完成一个NEDC(新欧洲行驶循环)测试工况后,4×4阵列射流最低温度达到了290.51 K,2×2阵列射流下的最低温度达到了293.34 K,比前者高了2.83 K,并且通过改变射流冷却系统的结构参数,观察到电池模组的平均温度呈现显著下降趋势。具体而言,当采用2×2射流阵列时,将射流孔的直径从1 mm增加至3 mm,可使电池模组的平均温度降低2.06 K;采用3×3射流阵列,在同样的孔径变化下(即从1 mm增至3 mm),平均温度的降幅进一步扩大至2.96 K;而当阵列配置达到4×4时,平均温度降低3.01 K,显示出最佳的冷却性能提升。 展开更多
关键词 电池热管理 空气射流冷却 相变材料 数值模拟
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风冷冲击射流与相变耦合的电池热管理数值分析
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作者 岳志强 高怀斌 +1 位作者 马建忠 马逾 《现代电子技术》 北大核心 2026年第4期21-26,共6页
针对圆柱型锂电池在应用中散热均匀性差的问题,提出了一种风冷冲击射流与相变材料(PCM)耦合的热管理系统。通过数值仿真分析了喷孔排列方式、喷孔直径及风速对电池最高温度和温度均匀性的影响,并对风冷冲击射流、相变材料和风冷耦合相... 针对圆柱型锂电池在应用中散热均匀性差的问题,提出了一种风冷冲击射流与相变材料(PCM)耦合的热管理系统。通过数值仿真分析了喷孔排列方式、喷孔直径及风速对电池最高温度和温度均匀性的影响,并对风冷冲击射流、相变材料和风冷耦合相变系统的冷却性能进行了对比。结果表明:在风速为2 m/s、喷孔直径为4 mm,且采用case2冲击板的工况下,电池最高温度降至40.06℃,最大温差控制在1.52℃;与常规风冷耦合PCM方案相比,风冷冲击射流与PCM耦合方案的最高温度降低了1.4℃,最大温差减少了2.03℃。 展开更多
关键词 锂离子电池 电池热管理系统 相变材料 风冷冲击射流 喷孔 冷却性能
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气刀压力调控下镀层冷却效应的数值模拟
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作者 王鑫 刘军祥 于庆波 《冶金能源》 北大核心 2026年第2期27-32,共6页
针对连续热镀锌工艺中气刀冷却效应与镀层厚度控制协同机制不明确的问题,建立了耦合镀层厚度模型的三维数值模拟。利用Fluent模拟气刀射流场,研究了不同进气压力下气刀射流对镀层厚度、温度分布和冷却效果的影响。结果表明:气刀射流的... 针对连续热镀锌工艺中气刀冷却效应与镀层厚度控制协同机制不明确的问题,建立了耦合镀层厚度模型的三维数值模拟。利用Fluent模拟气刀射流场,研究了不同进气压力下气刀射流对镀层厚度、温度分布和冷却效果的影响。结果表明:气刀射流的静压力呈高斯分布,切应力呈双峰特征,当进气压力由10.0 kPa升高至20.0 kPa时,镀层厚度从20.5μm减薄至17.4μm;进气压力升高显著增强对流换热效率,平均换热系数从413 W/(m^(2)·K)增大至540 W/(m^(2)·K),促使镀层表面平均温度降低8 K,沿Y方向首尾温差由32 K增大至46 K,且Z方向温度分布趋于均匀。该研究结果为优化镀层厚度和均匀性提供了理论依据,对提升高端镀锌板质量具有指导意义。 展开更多
关键词 热镀锌 气刀射流 镀层厚度 温度分布 冷却效果
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射流冲击冷却热力-水力性能多目标优化研究
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作者 关苏敏 丁若晨 +3 位作者 王宁波 叶青平 郑志美 邵双全 《制冷学报》 北大核心 2026年第1期80-87,共8页
探索高效、清洁、节能的冷却方案是数据中心脱碳的重要途径。本文提出一种变间距多射流直接芯片冷却方案,旨在提高传热系数并改善温度均匀性。研究了冷却剂流量、入口温度、针翅设计参数及射流孔间距对热阻、压降、温度标准差和努塞尔... 探索高效、清洁、节能的冷却方案是数据中心脱碳的重要途径。本文提出一种变间距多射流直接芯片冷却方案,旨在提高传热系数并改善温度均匀性。研究了冷却剂流量、入口温度、针翅设计参数及射流孔间距对热阻、压降、温度标准差和努塞尔数的影响。基于计算流体力学(CFD)和拉丁超立方采样实验设计生成用于构建代理模型的数据集,建立了以结构和热参数为输入,热阻、压降、温度均匀性为输出的人工神经网络模型,并采用基于均匀搜索的约束多目标优化算法(CMOES)求解优化模型。优化结果表明:最优设计在热力-水力性能上均优于初始设计及现有研究,具有良好工程应用前景。 展开更多
关键词 数据中心 射流冲击冷却 高热流密度 代理模型 多目标优化
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喷缝式镀后冷却风箱的阻力特性研究及结构优化
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作者 张建水 张庭君 +1 位作者 董强 肖斌 《轧钢》 北大核心 2026年第1期165-169,共5页
本文基于理论设计,结合模拟软件与现场应用实测数据及反馈,对缝式冲击射流在镀后冷却设计中的应用进了分析研究,总结出冷却风箱结构参数与风箱压力及速度系数的计算公式,可以精确风机选型,为工程设计提供了参考。同时,在相同能耗的情况... 本文基于理论设计,结合模拟软件与现场应用实测数据及反馈,对缝式冲击射流在镀后冷却设计中的应用进了分析研究,总结出冷却风箱结构参数与风箱压力及速度系数的计算公式,可以精确风机选型,为工程设计提供了参考。同时,在相同能耗的情况下,对风箱结构进行了优化,使其冷却能力最佳,达到提效节能的效果;同时,给出了最优结构参数的拟合公式,为该技术的工程推广应用提供了便捷可行的参考方案。 展开更多
关键词 冲击射流 带钢冷却 参数设计 节能优化 工程应用 连续退火 镀锌
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Modeling of Strip Temperature in Rapid Cooling Section of Vertical Continuous Annealing Furnace 被引量:3
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作者 WAN Fei WANG Yong-qin QIN Shu-ren 《Journal of Iron and Steel Research International》 SCIE CAS CSCD 2012年第11期27-32,共6页
The strip temperature is affected by many factors in rapid cooling section (RCS) of the vertical continuous annealing furnace (VCAF). They can he divided into four types: the physical properties of cooling gas, t... The strip temperature is affected by many factors in rapid cooling section (RCS) of the vertical continuous annealing furnace (VCAF). They can he divided into four types: the physical properties of cooling gas, the geometry characteristics of configuration of cooling equipment, the heat transfer between the strip and the cooling gas, and the conductivity of the strip. It aims to model the strip temperature in the cooling section based on the fundamental heat transfer theory and the four aspects factors. The model for transient Nusselt number is obtained by considering Reynolds number, Prandtl number and geometry characteristics of RCS. Then cooling model of the strip transient temperature is built by Nusselt number, heat transfer coefficient and heat conductivity of the strip. The results are compared with the data from production line. The comparisons indicate that the model can well predict cooling temperature of the strip. It is hoped that the proposed model can be used for design and control of the vertical continuous annealing furnace. 展开更多
关键词 rapid cooling jet impinging convection heat transfer coefficient
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燃料温度对正癸烷裂解气扩散火焰推举影响研究
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作者 赖重华 赵鸿海 +1 位作者 黄林远 黄胜 《四川大学学报(自然科学版)》 北大核心 2026年第1期168-174,共7页
喷气燃料高温裂解产物的燃烧特性直接关系到超燃冲压发动机的燃烧效率与运行安全性,而火焰推举现象作为扩散燃烧中的关键特征,对燃烧稳定性及污染物排放具有重要影响。正癸烷是喷气燃料的典型替代组分之一,本文利用耦联电加热流动管反... 喷气燃料高温裂解产物的燃烧特性直接关系到超燃冲压发动机的燃烧效率与运行安全性,而火焰推举现象作为扩散燃烧中的关键特征,对燃烧稳定性及污染物排放具有重要影响。正癸烷是喷气燃料的典型替代组分之一,本文利用耦联电加热流动管反应器与热伴流射流扩散燃烧器,对正癸烷在温度500~850℃的热裂解产物喷注燃烧特性进行了实验与理论分析研究。通过模拟计算了单组分乙烯与双组分正癸烷/乙烯的非反应混合过程。计算结果表明,在非反应的热空气与裂解气混合过程中,燃料温度上升带来的显焓提升对局部当量比的影响,远弱于其引发的裂解反应程度加剧对局部当量比的影响,后者是导致其局部当量比分布变化的主导因素。射流扩散火焰观测结果表明,随着燃料温度的升高,火焰的推举高度单调递减,对应滞燃时间均逐渐缩短。基于正癸烷及乙烯的燃烧反应机理计算的零维点火延迟时间,远大于实验中燃料接触空气后的滞燃时间,因此用稳定物种替代热裂解态燃料组成可能严重低估其反应活性。本研究为阐明高温燃料裂解-燃烧耦合过程的内在规律提供了实验支撑,也为发动机燃烧室的优化设计提供了理论依据。 展开更多
关键词 裂解气 正癸烷 热伴流火焰 火焰推举 主动冷却
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EXPERIMENTAL STUDY OF FLOW FIELDS IN THE VICINITY OF A FILM COOLING HOLE EXIT
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作者 Xu Hongzhou Liu Songling Xu Duchun(Department of Aeroengines and Thermal Power Engineering, NorthwestrnPolytechnical University ,Xi’an, China, 710072) 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1997年第2期91-97,共7页
For the first time, an important ingested flow phenomenon was discovered inexperiments at the film cooling hole exit. The trends of 3-D flow fie1ds and the fullnessfactor, Ci, were discussed in detail over a wide rang... For the first time, an important ingested flow phenomenon was discovered inexperiments at the film cooling hole exit. The trends of 3-D flow fie1ds and the fullnessfactor, Ci, were discussed in detail over a wide range of now parameters and the geometryof fan-shaped holes at this exit plane. It has been confirmed that the main reason of creat-ing longitudinal bound vortices is not the flow iri the hole but the mixing of mainstreamand jet at its exit. 展开更多
关键词 film cooling jet flow flow distribution VORTICES fullness factor
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Application of difference arithmetic in the continuous annealing process line cooling control at Baosteel
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作者 Lin Lijun 《Baosteel Technical Research》 CAS 2008年第4期35-38,共4页
Some of the main cooling processes and equipment that are currently being used in the continuous annealing process line (CAPL) at Baosteel are introduced, as well as their cooling control model techniques, the model... Some of the main cooling processes and equipment that are currently being used in the continuous annealing process line (CAPL) at Baosteel are introduced, as well as their cooling control model techniques, the modeling principium and their application results. With charts indicating the control trends in real processes, the powerful adjusting ability of the control models with process variable differences and their excellent control precision are shown in this study. 展开更多
关键词 roll quench gas jet cooling DIFFERENCE control gain heat transfer coefficient
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Flow Field Investigation in a Trapezoidal Duct with Swirl Flow Induced by Impingement Jets 被引量:3
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作者 LIU Haiyong QIANG Hongfu +1 位作者 LIU Songling LIU Cunliang 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第1期8-17,共10页
An enlarged model of trapezoidal duct near the leading-edge in the blade is built up. The effects of impingement jets, swirl flow, cross flow and effusion flow are considered. Experiments are performed to measure flow... An enlarged model of trapezoidal duct near the leading-edge in the blade is built up. The effects of impingement jets, swirl flow, cross flow and effusion flow are considered. Experiments are performed to measure flow fields in this confined passage and exit holes on one of its side walls. Cross flow and effusion flow are induced in the channel by the outflow of side exit hole (SEH) and film cooling hole (FCH), which are oriented on one end wall and bottom wall of the passage. Detailed flow structures are measured for two impingement angles of 35° and 45° with 6 combinations of outflow ratios. Results show that the small jets impinge the target wall effectively while the large jets contribute to inducing and impelling a strong counter-clockwise vortex in the upper part of the passage. Cross flow plays a dominate role for the flow structures in the passage and exit holes. It deflects jets, enhances swirl and deteriorates side exit conditions. Impingement angle is another significant factor for the flow characteristics. Its effect reveals more evidently with cross flow. Within the present test conditions, the mass flow rates and outflow positions of FCHs have no distinct effect on the main flow structures. 展开更多
关键词 flow fields leading edge impingement jets swirl flow film cooling cross flow
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High-Resolution Heat Transfer Coefficients Measurement for Jet Impingement Using Thermochromic Liquid Crystals 被引量:2
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作者 张靖周 李立国 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2001年第4期205-209,共5页
A high-resolution testing technique named liquid crystal thermography is used for the experimental study on jet array impingement to map out the distribution of heat transfer coefficients on the cooling surface. Effec... A high-resolution testing technique named liquid crystal thermography is used for the experimental study on jet array impingement to map out the distribution of heat transfer coefficients on the cooling surface. Effects of the impingement distance, the impinging hole arrangement and the initial crossflow on heat transfer characteristics are investigated. The thermal images show truly the features of local heat transfer for each jet impingement cooling. The applications of thermochromic liquid crystal are successful in the qualitative and quantitative measurement for heat transfer coefficients distribution. 展开更多
关键词 coolING Flow visualization Heat transfer coefficients jets Liquid crystals Thermography (imaging)
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Thermal Fluid Flow Transport Characteristics in Confined Channels with Two Dimensional Dual Jet Impingement
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作者 Senkal Caner Shuichi Torii 《材料科学与工程(中英文A版)》 2011年第5X期648-657,共10页
关键词 传输特性 射流冲击 密闭 热流体 通道 二维 状态方程 射流速度
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