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首页> 外文期刊>Journal of Mechanical Science and Technology >Analysis of laminar film condensation over vertical permeable hollow short fins
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Analysis of laminar film condensation over vertical permeable hollow short fins

机译:垂直可渗透空心短翅片上层流膜冷凝的分析

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摘要

Laminar falling film condensation over vertical short fin is analyzed. The fin is considered to be hollow and permeable in order to account for condensate suction towards its inner core. The present work accounts for the shear stress at the interface caused by the large velocity of the saturated vapor. The continuity, momentum, and energy equations for the film condensate are solved using an iterative and implicit finite-difference method. The condensate flow rate inside the fin is obtained using the conservation of mass principle and the Poiseuille flow equations. The one-dimensional fin equation model is used to relate the fin temperature to the condensate flow convection heat transfer coefficient. Various computational and numerical methods techniques such as advanced linearization and generations of best-fit correlations are implemented. This is to reduce significantly the number of iterations required for solution convergence as all of the aforementioned equations are coupled. It is found that the dimensionless total mass transfer rate increases slightly as vapor Reynolds number increases. It increases apparently as both suction Reynolds number and dimensionless suction length increase. For both large suction Reynolds number and large dimensionless suction length, the flow rate of the condensate in the falling film can be neglected compared to the total suction condensate flow rate. The fin thermal length increases as Reynolds number, dimensionless suction length, and Grashof number increase. This study shows that significant condensation mass flow rate enhancement ratios are obtainable (can be 18 folds) due to suction through a hollow super conductive fin.
机译:分析了垂直短翅片上的层状降膜凝结。该翅片被认为是中空的且可渗透的,以考虑向其内芯的冷凝物抽吸。本工作解释了由饱和蒸汽的大速度引起的界面处的剪切应力。使用迭代隐式有限差分法求解薄膜冷凝物的连续性,动量和能量方程。翅片内部的冷凝水流量是使用质量守恒原理和Poiseuille流量方程获得的。一维翅片方程模型用于将翅片温度与冷凝水对流传热系数联系起来。实现了各种计算和数值方法技术,例如高级线性化和最佳拟合相关性的生成。由于所有上述方程式都被耦合,这将大大减少求解收敛所需的迭代次数。发现随着蒸汽雷诺数的增加,无量纲的总传质速率略有增加。随着吸力雷诺数和无因次吸力长度的增加,吸力明显增加。对于较大的吸力雷诺数和较大的无量纲吸力长度,与总的吸气冷凝水流量相比,降膜中冷凝水的流量可以忽略不计。鳍片的热长度随着雷诺数,无因次吸力长度和格拉斯霍夫数的增加而增加。这项研究表明,由于通过空心的超导散热片进行抽吸,可获得明显的冷凝质量流速提高比(可以为18倍)。

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