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Three-Dimensional Numerical Simulation on Laminar Heat Transfer and Fluid Flow Characteristics of Strip Fin Surface With X-Arrangement of Strips

机译:带状X形排列的带状翅片表面层流传热与流动特性的三维数值模拟

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摘要

In this paper, a numerical investigation of air side performance of strip fin surface is presented. Three-dimensional numerical computation was made for a model of a two-row finned tube heat exchanger. The tube configuration is simulated with step-wise approximation, and the fin efficiency is also calculated with conjugated computation. Four types of fin surfaces were studied: A-the whole plain plate fin; B-the strip fin with strips located in the upstream part of the fin; C-the strip fin with strips located in the downstream part of the fin; and D-the strip fin with strips covering the whole fin surface. It is found that the strip fin with strips located in the downstream part of the fin surface (fin C) has higher heat transfer rate than that with strips in the upstream part (fin B) at the same conditions, white the pressure drop of fin C is a bit lower than that of fin B. A comprehensive performance comparison was conducted by using the goodness factor and the pumping power consumption per unit surface area. It is revealed that between the two strip fins the performance of fin C is better than fin B with same strip number. Detailed discussion is provided from the view point of synergy between velocity and temperature gradient. It is shown that the synergy between velocity and temperature field becomes worse in the downstream part of the fin surface, and it is this place that enhancement technique is highly needed. The strip location of fin C just fits this situation. The present numerical work provides useful information on where the enhancement element should be positioned.
机译:本文提出了带翅片表面空气侧性能的数值研究。对两排翅片管换热器的模型进行了三维数值计算。通过逐步逼近来模拟管的配置,并通过共轭计算来计算翅片效率。研究了四种类型的翅片表面:A-整个平板翅片; B-带状鳍,带位于鳍的上游; C-带状鳍,带位于鳍的下游部分; D-带状鳍片,带状物覆盖整个鳍片表面。发现在相同条件下,位于翅片表面下游部分(翅片C)的条状翅片的传热率高于位于上游部分(翅片B)的条状翅片的传热率。 C比翅片B低一些。通过使用优良系数和每单位表面积的泵浦功率消耗进行了全面的性能比较。结果表明,在两个带状翅片之间,相同条形数的翅片C的性能要优于翅片B。从速度和温度梯度之间的协同作用的角度提供了详细的讨论。结果表明,在翅片表面的下游部分,速度与温度场之间的协同作用变差,因此正是在这个地方急需增强技术。鳍C的条带位置恰好适合这种情况。本数字工作提供了有关增强元件应放置在何处的有用信息。

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