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空气射流冲击下柱鳍热沉散热特性实验研究 被引量:2
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作者 涂福炳 周孑民 曾文辉 《湖南科技大学学报(自然科学版)》 CAS 北大核心 2008年第2期41-46,共6页
电子系统微型化、大功率的发展趋势,以及对系统性能和可靠性的需求,要求电子元件具有更为强大的散热性能.空气射流冲击,尤其与其他表面强化传热方式的结合是一个很好的选择,采用这种散热方式几乎能达到与液体冷却相当的散热能力.选用3... 电子系统微型化、大功率的发展趋势,以及对系统性能和可靠性的需求,要求电子元件具有更为强大的散热性能.空气射流冲击,尤其与其他表面强化传热方式的结合是一个很好的选择,采用这种散热方式几乎能达到与液体冷却相当的散热能力.选用3个不同肋高的矩形柱鳍热沉对空气射流冲击矩形柱鳍热沉进行传热特性的实验研究.首先,分别获得了这3个热沉的热阻(θab)随Re数及H/D变化的实验数据和对应这3个热沉的模拟芯片表面的平均努塞尔数(Nu)随Re数及H/D变化的实验数据;其次,选用合适的函数形式对实验数据采用最小二乘法拟合,得到了此实验条件下关于Re、H/D及肋片高度Hf的准数方程.实验结果表明,随Re或H/D的增大而减小,但当Re或H/D增大到一定程度时,θab减小的幅度就不再明显;Nu数关于Re、H/D及肋片高度Hf的实验公式,其相对误差小于9%;在3159≤Re≤15798的范围内,这种冷却方式下的对流换热系数可达500~1100W/(m·2K). 展开更多
关键词 空气射流冲击 柱鳍热沉 努塞尔数 热阻
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圆喷嘴亚声速空气冲击射流壁面压力规律实验研究 被引量:2
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作者 申正 叶骞 《液压与气动》 北大核心 2017年第11期54-59,共6页
针对圆形喷嘴亚声速空气冲击射流,对多种不同工况下壁面压力分布规律进行了实验研究,实验结果表明壁面压力规律近似遵循高斯分布。为了得到精确的分布关系式,首先建立了高斯分布中压力分布半宽度与喷距的关系,在此基础上对不同工况下的... 针对圆形喷嘴亚声速空气冲击射流,对多种不同工况下壁面压力分布规律进行了实验研究,实验结果表明壁面压力规律近似遵循高斯分布。为了得到精确的分布关系式,首先建立了高斯分布中压力分布半宽度与喷距的关系,在此基础上对不同工况下的高斯分布进行修正,给出修正关系式,有效地降低了单纯用高斯分布的误差。最后给出了压力分布范围与喷距的关系,为实际使用提供帮助。 展开更多
关键词 空气射流冲击 亚声速 壁面压力分布 压力分布范围
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射流冲击下矩形柱鳍热沉结构优化
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作者 涂福炳 武荟芬 +3 位作者 周孑民 曾文辉 刘亮 贾煜 《中南大学学报(自然科学版)》 EI CAS CSCD 北大核心 2012年第3期1171-1178,共8页
采用实验与数值计算相结合的方法对空气射流冲击下的矩形柱鳍热沉的肋片结构进行优化研究。对不同肋高和肋宽的矩形柱鳍热沉的热阻进行实验研究,并选用标准的kε湍流模型进行数值计算分析。研究结果表明:热阻随喷口雷诺数Re或喷口高径比... 采用实验与数值计算相结合的方法对空气射流冲击下的矩形柱鳍热沉的肋片结构进行优化研究。对不同肋高和肋宽的矩形柱鳍热沉的热阻进行实验研究,并选用标准的kε湍流模型进行数值计算分析。研究结果表明:热阻随喷口雷诺数Re或喷口高径比H/D的增大而减小,但Re或H/D增大到一定程度时,热阻减小的幅度就不再明显;当热沉肋高范围为0.3≤Hf/L≤0.42、肋片宽度为Df/L=0.1时,热沉的散热能力与散热经济性之间能达到较好的平衡。将模拟结果与实验结果进行比较,相对误差在10%以内。 展开更多
关键词 空气冲击射流 矩形柱鳍热沉 热阻 数值模拟 肋片优化
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Supersonic Moist Air Jet Impingements on Flat Surface 被引量:2
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作者 ALAM Miah Md.Ashraful MATSUO Shigeru SETOGUCHI Toshiaki 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第1期51-59,共9页
Pronounced aeroacoustic resonances are exhibited in the flow field where a jet emerges from an orifice or a nozzle and impinges on a solid surface. One instance where such resonances are produced is in a high speed je... Pronounced aeroacoustic resonances are exhibited in the flow field where a jet emerges from an orifice or a nozzle and impinges on a solid surface. One instance where such resonances are produced is in a high speed jet impingement, such as in the space launch vehicle systems, jet-engine exhaust impingement, and in the short take-off and vertical landing (STOVE) aircraft, etc. A highly unsteady flowfield leading to a drastic increase of noise level with very high dynamic pressure and thermal loads are noticed on nearby surfaces results dramatic lift loss, severe ground erosion and hot gas ingestion to the inlet in the jet engines. This highly unsteady behavior of the im- pinging jets is due to a feedback loop between the fluid and acoustic fields. In actual jet flow, the working gas may contain condensable gas such as steam or moist air. In these cases, the non-equilibrium condensation may occur at the region between nozzle exit and an object. The jet flow with non-equilibrium condensation may be quite different from that without condensation. Therefore, in this study, the effect of the non-equilibrium condensation of moist air on the axisymmetric under-expanded supersonic impinging jet on a vertical flat plate was investigated numerically. 展开更多
关键词 compressible flow SUPERSONIC IMPINGING non-equilibrium condensation OSCILLATION
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Thermal Characteristics of Air-Water Spray Impingement Cooling of Hot Metallic Surface under Controlled Parametric Conditions
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作者 Santosh Kumar Nayak Purna Chandra Mishra 《Journal of Thermal Science》 SCIE EI CAS CSCD 2016年第3期266-272,共7页
Experimental results on the thermal characteristics of air-water spray impingement cooling of hot metallic surface are presented and discussed in this paper.The controlling input parameters investigated were the combi... Experimental results on the thermal characteristics of air-water spray impingement cooling of hot metallic surface are presented and discussed in this paper.The controlling input parameters investigated were the combined air and water pressures,plate thickness,water flow rate,nozzle height from the target surface and initial temperature of the hot surface.The effects of these input parameters on the important thermal characteristics such as heat transfer rate,heat transfer coefficient and wetting front movement were measured and examined.Hot flat plate samples of mild steel with dimension 120 mm in length,120 mm breadth and thickness of 4 mm,6 mm,and 8mm respectively were tested.The air assisted water spray was found to be an effective cooling media and method to achieve very high heat transfer rate from the surface.Higher heat transfer rate and heat transfer coefficients were obtained for the lesser i.e,4 mm thick plates.Increase in the nozzle height reduced the heat transfer efficiency of spray cooling.At an inlet water pressure of 4 bar and air pressure of 3 bar,maximum cooling rates670℃/s and average cooling rate of 305.23℃/s were achieved for a temperature of 850℃ of the steel plate. 展开更多
关键词 air-water spray transient temperature cooling rate plate thickness
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