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Numerical Analysis of Fluid Flow and Heat Transfer in Wavy and Hybrid-Slit-Wavy (HSW) Fin-and-Tube Heat Exchangers

机译:波浪杂交狭窄(HSW)翅片管热交换器流体流动和热传递的数值分析

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This numerical study pertains to characterizing flow and heat transfer interactions for an interrupted fin design with wavy profile in compact tube-and-fin heat exchanger. Although designs with similar concept is prevalent in the HVAC&R industry not much literature exists on the subject combining wavy fins with periodic interruptions. Presently sinusoidal wavy fin is combined with slit fins to investigate thermal-hydraulic performance relative to an un-interrupted fin design. This fin is referred to as Hybrid Slit Wavy (HSW) fin in this work. Commercial Computational Fluid Dynamics (CFD) software is used for 3D numerical solution of the complete Navier-Stokes and energy equations in the heat exchanger to study flow physics and predict performance. The modeling approach is first validated with available test data from the literature on a wavy (Herringbone profile) fin heat exchanger. The predicted friction factor f was within 12% and the Colburn j-factor was within 7% of the reported test data over a Reynolds number range of 350-6500. In the case of the HSW fin it was found that the air-side heat transfer is enhanced by about 20-39% relative to the baseline un-interrupted fin with an associated pressure drop penalty of 20-38%. The area goodness factors of the HSW fins are up to 4% higher compared to the wavy fins at various operating conditions indicative of favorable trade-off. It is further established that the local flow pattern including boundary layer modifications, wake structures and enhanced flow mixing correlates strongly with local Nusselt number distribution.
机译:该数值研究涉及具有紧凑型管和翅片热交换器中的波状型材的中断翅片设计的流动和传热相互作用。虽然具有类似概念的设计在HVAC&R行业中普遍存在的文学中,但主体存在与周期性中断的波浪鳍相结合。目前SinUnoidal波浪翅片与狭缝翅片相结合,以研究相对于未中断翅片设计的热液压性能。在这项工作中,该鳍片被称为混合狭缝波浪(HSW)鳍片。商业计算流体动力学(CFD)软件用于完整的Navier-Stokes和热交换器中的能量方程的3D数值解决方案,以研究流量物理和预测性能。建模方法首先用来自波浪(人字带轮廓)翅片热交换器的文献中的可用测试数据验证。预测的摩擦系数F在12%以内,CONBurn J-因子在报告的测试数据的7%内通过350-6500的雷诺数范围内。在HSW鳍片的情况下,发现空气侧传热相对于基线未中断翅片的增强约20-39%,具有20-38%的相关压降。与各种操作条件的波浪翅片相比,HSW鳍片的面积良好因素高达4%,指示有利的折衷。还建立了包括边界层修改,唤醒结构和增强流动混合的局部流动模式与局部露珠数分布强烈地相关。

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