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Numerical Investigations on Enhancement of Heat Transfer in a Compact Fin-and-Tube Heat Exchanger Using Delta Winglet Type Vortex Generators

机译:三角翼小涡旋发生器强化紧凑型翅片管式换热器传热的数值研究

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摘要

Three dimensional flow and heat transfer in a compact fin-tube cross flwo heat exchanger have been modeled as the flow in a rectangular channel with built-in cylindrical obstacles. The flow past a tube bank has been simulated by a spacewise periodic fully developed flow in a computational domain consisting of a channel element with one tube. Flow and temeprature fields in this element and in another element with two in-line tubes have been computed forml the numerical solution of three dimensinal Navier-Stokes and energy equations. Comparison of results show that at low Reynolds number (~400) the Nusselt number in the neighbourhood of the seond tube of a two tube in-line configuration is close to the Nusselt number for spacewise periodic fully developed flow. Computatioanl results also shwo poor heat transfer in the wake region. In the presence of the winglet type longitudinal vortex generatiors int ehwake behind the cylinder, heat transfer in this region is enhanced signficantly. Results show increases in average Nusselt number due to the vortex generators can be between 20 and 50 percent in the Reynolds number rnage of 400 and 1200. A factor, defined as the ratio of increase in Nusselt number to increase in fricition factor, of 0.65 to 0.78 can be obtained, over the range of Reynolds number mentioned above.
机译:紧凑型翅片管横向流动换热器中的三维流动和传热已建模为带有内置圆柱形障碍物的矩形通道中的流动。经过管束的流动已通过在计算域中的空间周期性完全展开的流动进行了模拟,该计算域由带有一根管的通道元素组成。计算了该元件以及另一个具有两个直管的元件中的流动和温度场,以计算三个二维Navier-Stokes和能量方程的数值解。结果比较表明,在低雷诺数(〜400)时,两管直列构造的第二管邻管中的Nusselt数接近于空间周期性完全展开流的Nusselt数。计算结果也使尾流区域的传热不佳。在圆柱体后面存在小翼型纵向涡流发生器时,该区域的热传递显着增强。结果显示,在400和1200的雷诺数范围内,由于涡流发生器而导致的平均Nusselt数增加可以在20%到50%之间。一个因子(定义为Nusselt数增加与摩擦因子增加的比)为0.65至在上述雷诺数的范围内,可以获得0.78。

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