共查询到19条相似文献,搜索用时 156 毫秒
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流速对混合蒸汽Marangoni凝结换热影响的实验研究 总被引:1,自引:0,他引:1
本文在蒸汽压力为47.36 kPa的条件下,通过实验研究了不同蒸汽流速(u=2、4、5 m/s)下纯水和不同酒精浓度水-酒精混合蒸汽沿重力方向流过竖直紫铜平板表面上的凝结换热特性,并实现了实验的可视化,同时分析了不同蒸汽流速下造成Marangoni凝结换热特性差异的原因.实验及分析结果表明,在相同蒸汽浓度、蒸汽压力和表面过冷度条件下,高流速下的凝结换热系数比低流速的大.且蒸汽流速对凝结换热的影响因混合蒸汽酒精浓度的不同而不同,低浓度0.5%和高浓度50%时流速的增加对凝结换热特性的影响较小,而在中间浓度2%时凝结换热强度随流速的增加明显. 相似文献
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蒸汽压力对Marangoni凝结换热特性的影响 总被引:4,自引:3,他引:1
本文研究了蒸汽压力对水-酒精混合蒸汽竖直平板表面凝结换热特性的影响.搭建了具有高气密性的Marangoni凝结换热实验台,分别针对不同压力(31.16 kPa,47.36 kPa,84.53 kPa)、不同表面过冷度(表面过冷度范围2-32℃)的纯水、水-酒精混合液(气相酒精质量百分比浓度为2.28%,5.1%,51%)和酒精进行了换热特性的实验研究,实验结果表明混合蒸汽在相同流速和浓度下凝结表面传热系数随压力的升高而升高,分析认为这是因为相平衡压力的提高会导致凝结液量增加和凝结液平均温度提高,而使凝结汽液界面的表面张力提高,进一步增强了Marangoni效应的影响,从而使凝结表面传热得到加强. 相似文献
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本文研究了温度梯度对不同浓度水-酒精混合蒸气的Marangoni凝结的影响.搭建了具有高气密性的实验台,设计了凝结表面存在温差的实验块.在低于大气压力(31.2 kPa,47.4 kPa,84.5 kPa)的条件下,对8个浓度(0%~50%)混合蒸气进行了实验研究并实现可视化.实验结果表明温度梯度在低过冷度(<10 K)下,提高了低浓度(0.5%,1%)的水-酒精混合蒸气的换热系数.分析认为是因为表面温差带来了表面张力的差异,促使液膜内扰动增大,减少了凝结液膜热阻的缘故. 相似文献
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水和酒精Marangoni凝结换热特性研究 总被引:7,自引:2,他引:5
本文首先构造了一个在常温水冷却时,纯水蒸汽凝结时表面温度差可以达到11℃的黄铜试件。利用该试件在蒸汽流速为0.3m/s时,进行了不同浓度水-酒精混合蒸汽以及纯水蒸汽的凝结换热特性和凝结状态的实验研究。实验结果表明:由于凝结表面存在温度差,水-酒精混合蒸汽出现珠状凝结,凝结换热系数最大可以达到纯水蒸汽凝结的2.8倍;混合蒸汽凝结换热系数随表面过冷度减小而增加,并在较小过冷度时出现陡增;凝结换热量随表面过冷度增加存在最大值;观察得出了不同表面过冷度下不同酒精浓度时的凝结状态。 相似文献
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This article directly investigates the effect of a cooling medium's coolant temperature on the condensation of the refrigerant R-134a. The study presents an experimental investigation into condensation heat transfer, vapor quality, and pressure drop of R-134a flowing through a commercial annular helicoidal pipe under the severe climatic conditions of a Kuwait summer. The quality of the refrigerant is calculated using the temperature and pressure obtained from the experiment. Measurements were performed for refrigerant mass fluxes ranging from 50 to 650 kg/m2s, with a cooling water flow Reynolds number range of 950 to 15,000 at a fixed gas saturation temperature of 42°C and cooling wall temperatures of 5°C, 10°C, and 20°C. The data shows that with an increase of refrigerant mass flux, the overall condensation heat transfer coefficients of R-134a increased, and the pressure drops also increased. However, with the increase of mass flux of cooling water, the refrigerant-side heat transfer coefficients decreased. Using low mass flux in a helicoidal tube improves the heat transfer coefficient. Furthermore, selecting low wall temperature for the cooling medium gives a higher refrigerant-side heat transfer coefficient. 相似文献
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An experimental study of condensation heat transfer characteristics of flow inside horizontal micro-fin tubes is carried out using R410A, R22, and R32 as the test fluids. This study especially focuses on the influence of heat transfer area upon the condensation heat transfer coefficients. The test sections were made of double tubes using the counter-flow type; the refrigerants condensation inside the test tube enabled heat to exchange with cooling water that flows from the annular side. The saturation temperature and pressure of the refrigerants were measured at the inlet and outlet of the test sections to defined state of refrigerants, and the surface temperatures of the tube were measured. A differential pressure transducer directly measured the pressure drops in the test section. The heat transfer coefficients and pressure drops were calculated using the experimental data. The condensation heat transfer coefficient was measured at the saturation temperature of 48°C with mass fluxes of 50–380 kg/(m2s) and heat fluxes of 3–12 kW/m2. The values of experimental heat transfer coefficient results are compared with the predicted values from the existing correlations in the literature, and a new condensation heat transfer coefficient correlation is proposed. 相似文献
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In this study, condensation of pure refrigerant R134a vapor inside a smooth vertical tube was experimentally investigated. The test section was made of a copper tube with inside diameter of 7.52 mm and length of 1 m. Experimental tests were conducted for mass fluxes in the range of 20–175 kg/m2s with saturation pressure ranging between 5.8 and 7 bar. The effects of mass flux, saturation pressure, and temperature difference between the refrigerant and tube inner wall (ΔT) on the heat transfer performance were analyzed through experimental data. Obtained results showed that average condensation heat transfer coefficient decreases with increasing saturation pressure or temperature difference (ΔT). In addition, for the same temperature difference (ΔT), heat can be removed from the refrigerant at a higher rate at relatively low pressure values. Under the same operating conditions, it was shown that average condensation heat transfer coefficient increases as mass flux increases. Finally, the most widely used heat transfer coefficient correlations for condensation inside smooth tubes were analyzed through the experimental data. The best fit was obtained with Akers et al.'s (1959) correlation with an absolute mean deviation of 22.6%. 相似文献
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In this study, condensation of pure refrigerant R134a vapor inside a vertical 18° helical microfin tube was experimentally investigated. Tests were performed at saturation pressure of 5.7–5.9 bar with mass fluxes of 20–100 kg/m2s and heat fluxes of 1.7–5.3 kW/m2. The effects of mass flux and the temperature difference between the refrigerant and tube wall (ΔT) on the heat transfer performance were analyzed throughout experimental data. For experiments in which ΔT is more than 2.5°C, the average condensation Nusselt number showed a tendency to be independent from ΔT. Heat transfer enhancement ratio was found to be 1.59–1.71, which is always higher than the heat transfer area enhancement factor (1.55). Fins always act as a turbulence promoter in the given experimental data range. Finally, the most widely used heat transfer coefficient correlations for condensation inside microfin tubes were analyzed through the experimental data. Best fit was obtained with Yu and Koyama's correlation with an absolute mean deviation of 17% and Kedzierski and Goncalves's correlation with an absolute mean deviation of 19%. 相似文献
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直喷发动机燃油喷雾撞击壁面形成油膜,导致燃烧效率降低,颗粒物排放增加。伴随撞壁的动态传热过程对油膜蒸发具有重要影响。本文针对正戊烷、甲醇、甲醇汽油混合燃料瞬态喷雾撞击壁面,研究了不同条件下蒸发性对燃油瞬态喷雾撞击壁面动态传热影响。结果表明,提高喷油温度可促进燃油雾化,增大喷油压力或降低喷油距离可提高液滴撞壁强度,缩短液膜存在时间。撞壁瞬态温度与热流密度动态变化特征受燃油蒸发性与喷雾条件联合影响。 相似文献