共查询到19条相似文献,搜索用时 78 毫秒
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李林星陈威祝啸凌娟娟 《低温与超导》2015,(10):67-73
为了分析泡沫金属在狭缝射流冲击泡沫金属强化换热的作用,在计算流体力学(CFD)的基础上,采用数值模拟的方法,对影响换热的一系列因素做了详细的研究。在模型中泡沫金属材质为纯铜,尺寸是定值,通过改变喷嘴内空气速度v、泡沫金属孔隙率φ、喷嘴宽度W与泡沫金属的高度H的比值、喷嘴到泡沫金属上表面的高度C与泡沫金属的高度H的比值,来分析各个因素对热表面换热系数、泡沫金属内温度分布和流线分布等因变量的影响。 相似文献
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薄液膜蒸发由于其优良的传热特性而被广泛应用于工业领域。在流动液膜上表面覆盖铜质泡沫金属,并耦合空气射流冲击,能够进一步强化传热。多孔泡沫金属提供的毛细驱动力能够有效控制流动液膜的厚度以避免干涸,同时多孔材料特殊的固体骨架构造可以扩大固液、气液传热面积。为了研究射流冲击条件下多孔介质覆盖流动液膜的传热特性,本文通过实验方法,对包括液膜流速Vf、空气射流速度Va、液膜厚度δf和多孔介质孔隙率ε在内的影响因素进行分析,研究并对比这些因素对加热壁面温度Tw、表面传热系数hw以及传热系数提升率的影响。 相似文献
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自耦合射流冲击冷却的数值计算 总被引:2,自引:0,他引:2
本文利用动网格技术对两维自耦合射流冲击冷却恒热流壁面进行了数值模拟,腔体底面具有一定的运动规律,每个时间步网格会重新划分。通过对流场和温度场的分析,得出以下结论:自耦合射流是零质量射流,射流的截面速度分布具有自相似性。涡对的平移和破碎影响了温度场的分布,从而冲击靶面温度最低点不是出现在射流驻点区,而是对应于涡对破碎、紊流度最大的位置。 相似文献
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The characteristics of supersonic impinging jets are investigated using Particle Image Velocimetry (PIV). The purpose of the experiments is to understand the jet induced forces on STOVL aircraft while hovering close to the ground. For this purpose, a large diameter circular plate was attached at the nozzle exit. The oscillations of the impinging jet generated due to a feedback loop are captured in the PIV images. The instantaneous velocity field measurements are used to describe flow characteristics of the impinging jet. The important flow features such as oscillating shock waves, slipstream shear layers and large scale structures are captured clearly by the PIV. The presence of large scale structures in the impinging jet induced high entrainment velocity in the near hydrodynamic field, which resulted in lift plate suction pressures. A passive control device is used to interfere with the acoustic waves travelling in the ambient medium to suppress the feedback loop. As a consequence, the large scale vortical structures disappeared completely leading to a corresponding reduction in the entrainment. 相似文献
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This article presents an experimental investigation on the merging probability of buoyancy-controlled jet flames. Two rectangular jet nozzles with different aspect ratios and heat release rates were studied in the open space. The nozzles of the same area with dimensions of 1.5 × 24, 3 × 12, and 6 × 6 mm were used in this article. It is found that the merging probability increases with the heat release rate and decreases with the space between these two nozzles. A model to predict the merging probability has been developed, which is proportional to a dimensionless parameter linearly within a certain scope. 相似文献
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H.K. Tanna 《Journal of sound and vibration》1977,50(3):405-428
The characteristics, both spectral and directivity, of turbulent mixing noise in the far field from subsonic and fully-expanded supersonic jet flows have been studied experimentally over an extensive envelope of jet operating conditions (jet exit velocity and temperature). The measurements were conducted in an anechoic room which provides a free-field environment. The results are presented in a systematic manner, and the observed trends and dependencies are discussed in detail. In particular, the changes in detailed jet noise features with varying velocity and exhaust temperature are assessed independently. Empirical prediction schemes or comparisons with recent theoretical investigations are not attempted here. However, the isothermal jet noise results are compared with those predicted by the freely-convecting quadrupole theories (that is, in the absence of any mean flow shrouding effects). The discrepancies between this model and the measurements, many of which have been recently shown to occur due to the presence of mean velocity and temperature gradients surrounding the sources, are obtained accurately over all jet operating conditions of interest. 相似文献
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H.K. Tanna 《Journal of sound and vibration》1977,50(3):429-444
The characteristics of the sound field of shock-containing under-expanded jet flows are studied by measuring the noise from a convergent nozzle operated over an extensive envelope of supercritical jet operating conditions. The measurements were conducted in an anechoic facility. They are complementary to the turbulent mixing noise experiments (described in Part I) for subsonic and fully-expanded (shock-free) supersonic jets. The overall results from shock-containing jets are compared directly with the corresponding results from shock-free jets, and the effects of nozzle pressure ratio and jet exhaust temperature on broadband shock-associated noise are assessed independently. For a supersonic jet, the regimes of jet operating conditions, observer angles, and frequencies over which the sound field is dominated by shock-associated noise are identified. Finally, the spectral results are compared in a preliminary manner with the spectra predicted by an existing theoretical model, and good agreement is obtained in most cases. 相似文献
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在HIRFL-CSR实验环电子冷却装置上采用了独立的高精度螺线管串联产生纵向磁场的设计,获得很高的冷却段磁场平行度。使用霍尔片测量磁场的分布,使用磁针测磁方法测量冷却段磁场的磁轴偏角,并根据测量及计算结果对单个线圈磁轴进行微调。测量及调试结果表明,在施加电流为额定电流的一半时,冷却段磁感应强度为0.078 T,剩余磁场小于2×10-4 T,磁场不平行度小于1×10-4,达到了预期的设计目标。 相似文献
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在HIRFL-CSR实验环电子冷却装置上采用了独立的高精度螺线管串联产生纵向磁场的设计,获得很高的冷却段磁场平行度。使用霍尔片测量磁场的分布,使用磁针测磁方法测量冷却段磁场的磁轴偏角,并根据测量及计算结果对单个线圈磁轴进行微调。测量及调试结果表明,在施加电流为额定电流的一半时,冷却段磁感应强度为0.078 T,剩余磁场小于2×10-4 T,磁场不平行度小于1×10-4,达到了预期的设计目标。 相似文献
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