共查询到18条相似文献,搜索用时 187 毫秒
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对发生在吸收器内的二元溶液两相流动传热传质过程进行了深入细致的描述。结合实际运行情况,将流动过程划分为3个区域,给出了不同区域的控制微分方程,建立了溶液滴状降膜吸收模型。基于Matlab平台进行求解,分析了水平管束式吸收器溶液温度、浓度的变化以及不同结构参数及运行工况下,溶液质量流量、润湿率WR、蒸发温度等变量对吸收器蒸气吸收能力、吸收器热负荷及蒸发器制冷量的影响。所得结果对于吸收器等热力部件的结构计算具有一定的参考作用。 相似文献
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垂直管外溴化锂溶液降膜吸收的传热传质模型研究 总被引:4,自引:0,他引:4
通过对溴化锂吸收式制冷机中垂直管外降膜吸收过程特点的分析,建立了吸收过程中传热传质相互耦合的数学物理模型,并在此基础上,进一步提出了溶液多次布液降膜吸收的模型;并对吸收过程中液膜流动、传热传质进行了分析,得出的结论可以为吸收器的设计和实际运行的优化提供一定的理论指导。 相似文献
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根据溴化锂吸收式制冷机吸收器中传热传质的物理模型和数学模型,通过计算分析了吸收器的布置方式和溶液再循环倍率对其吸收性能的影响,认为在所计算的三种布置方式中,以冷却水下进上出方式的总吸收效果最好,出液浓度和温度最低;计算结果还表明,溶液再循环倍率越大,吸收器的吸收性能越差,所以在满足喷淋密度的情况下应尽可能地减小溶液再循环倍率。 相似文献
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板式膜反转降膜吸收器的设计研究 总被引:3,自引:0,他引:3
建立并求解了板式膜反转降膜吸收过程的数学模型。通过计算比较了不同反转次数和分段位置降膜吸收过程的吸收效果,确立了最佳反转次数和分段位置。这项设计研究可作为板式膜反转降膜吸收器设计的理论依据,并为今后这类传热传质设备的工程设计、开发和应用提供一定的理论参考。 相似文献
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叶片前缘气膜冷却数值模拟 总被引:4,自引:0,他引:4
为了研究叶片前缘区域的换热特性,采用非结构化网格和realizable紊流模型,求解三维N-S方程,对前缘带有一排冷气孔的涡轮叶片进行了换热特性的数值模拟.分析了不同动量比,湍流度,孔间距及径向角下冷气射流的运动规律,换热分布以及冷效分布特点.结果表明,当动量比Ⅰ大于1时,在相同孔型下,动量比越高,冷效越大.在相同动量比下,孔间距越小,冷效越大.但动量比,孔间距及径向角对换热系数影响不大.当湍流度增加时,换热系数增加而冷效降低.沿展向,气膜孔中心区域冷效较高,两孔之间区域较低;而换热系数则相反,气膜孔中心区域换热系数较小,两孔之间区域较大. 相似文献
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Kwang Soo Kim Won Tae Kim Ki Baik Lee 《Journal of Mechanical Science and Technology》1998,12(1):132-142
Present study is concerned with forced convective heat transfer of the channel flow with line arrays of heated electronic
components mounted on a printed circuit board. For the assessment of thermal performance in channel flows, three separate
variables are used:channel spacing, row number of the component, and inlet air velocity. The thermal characteristics of a
component due to own power and upstream air heated by components were studied. The experimental results were compared with
those of numerical solution for various conditions: surface temperature of the components, adiabatic temperature rise, and
heat transfer coefficient. The experimental results agree well with the numerical solutions. The study shows that the adiabatic
heat transfer coefficient is significantly affected by the inlet velocity in channel flow and less dependent on the channel
spacing and row number, except for the case ofH/B=3.3. While reviewing the previous literatures, it is found that a little difference in the correlation between Nu and Re
is due to the different geometric ratio of the packaged components. 相似文献
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Both the mass flow rate and heat transfer characteristics are significant factors to the flow behavior of the high-pressure air; however, they are not easy to be obtained by analytical model during discharge and charge processes. In this paper, the mass flow rate characteristics of high-pressure pneumatic components (HPPC) are measured by a compounding approach; two components under test with the same geometry and dimension are needed to be connected in series. Both the effective cross-section area and critical pressure ratio of HPPC are determined accurately, and only the pressure variation and the steady-state temperature of air in the chamber are utilized. The compared results between experimental and simulation data show that the accuracy of the measured effective cross-section area and critical pressure ratio of the HPPC is high when the sonic and adiabatic releasing time is less than 2 s. And then, a new combined method of calculating the heat transfer coefficient during discharging and charging processes for the high-pressure air is proposed. The computational fluid dynamics (CFD) method is used to illustrate the intensity of heat exchange between the high-pressure air inside the chamber and outer atmosphere. The dynamic flow behavior is analyzed based on the tested flow rate characteristics of HPPC, mixed heat transfer theory and numerical results. The results show that the heat-transfer coefficient during charge process is much greater than discharge process, and the forced convection heat exchange happened owing to the strong “air agitation” during the charge process. The experimental results also validate that the proposed method of calculating the transient heat transfer coefficient is more reasonable to describe the heat transfer behavior. The findings may also have general implication in the development of the design and analysis of the high-pressure pneumatic system. 相似文献
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根据涡旋压缩机的运转规律,得到了绝热状态涡旋压缩机非定常流动的数值模拟计算方法;对涡旋压缩机理论计算模型进行网格无关性验证、动网格重构验证,保证其数值模拟计算结果的准确性.得到了涡旋压缩机工作过程的压力场、温度场、速度场分布规律,得到其工作过程曲线与各工作腔的泄漏规律,并与理论绝热过程进行对比,验证了所采用的数值模拟计算方法的正确可行性.进而探究考虑流热耦合传热的涡旋压缩机工作过程的数值模拟计算方法,提出通过合理地设置壁面热力条件参数实现涡旋压缩机达到热力平衡状态的数值模拟计算方法. 相似文献
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Hyo-Min Jeong Han-Shik Chung Sang-Chul Lee Tae-Woo Kong Chung-Seub Yi 《Journal of Mechanical Science and Technology》2006,20(4):545-553
Generally, the temperature drop under 0°C on vaporizer surface creates frozen dews. This problem seems to increase as the
time progress and humidity rises. In addition, the frozen dews create frost deposition. Consequently, heat transfer on vaporizer
decreases because frost deposition causes adiabatic condition. Therefore, it is very important to solve this problem. This
paper aims to study of the optimum design of used vaporizer at local LNG station. In this paper, experimental results were
compared with numerical results. Geometries of numerical and experimental vaporizers were identical. Studied parameters of
vaporizer are angle between two fins (Φ) and fin thickness (THF). Numerical analysis results were presented through the correlations between the ice layer thickness (THICE) on the vaporizer surface to the temperature distribution of inside vaporizer (TIN), fin thickness (THF), and angle between two fins (Φ). Numerical result shows good agreement with experimental outcome. Finally, the correlations
for optimum design of vaporizer are proposed on this paper. 相似文献