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Analytic study on pressure drop and heat transfer characteristics for low reynolds number flow in spirally finned tubes

机译:螺旋翅片管中低雷诺数流量压降和传热特性的分析研究

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Analytic solutions of the velocity and temperature profiles for a low Reynolds number flow in a spirally finned tube are obtained. The cross-sectional shape of the unit channel of the spirally finned tube is described by an annular sector with an inner radius r_i, an outer radius r_0, and an apex angle 2α. The channel is twisted about its longitudinal axis with a twist length H. To simplify the problem, it is assumed that the swirling effect is negligible, which is valid for low Reynolds number flows. By using an appropriate coordinate transformation, the fully-developed flow in the spirally finned tube can be treated as a quasi-2-dimensional flow. The perturbation method is used to solve the transformed momentum and energy equations for forced convection in the tube subject to the uniform heat flux condition. The Poiseuille and Nusselt numbers are obtained by using the analytic solutions for the velocity and temperature profiles. The values of /Re and Nu are presented in terms of the geometrical parameters, 2α, R_i = r_i/r_0, and w = 2πr_0/H. The results obtained from the analytic solutions show good agreement with numerical results for ω ≤ 0.5 and Re < 21/ω. These analytic solutions are useful for optimizing the thermal performance of the spirally finned tube under various constraints. To illustrate their usefulness, the thermal resistance of a spirally finned tube under the constraint of fixed pumping power is evaluated. Based on the analytic solutions, the optimum fin geometry for which a minimum thermal resistance is attained can be analytically determined for a given non-dimensional pumping power. Furthermore, correlations of the optimum fin number and optimum twist ratio are presented in this study. According to the results, for relatively low pumping power conditions (P_(pump)~*≤ P_(pump,crit)~*). the straight finned tube has better thermal performance than that of the spirally finned tube, and the optimum fin number increases as the pumping power increases. On the other hand, For relatively high pumping power conditions, (p_(pump)~*> P_(pump,crit)~*),the spirally finned tube has better thermal performance than that of the straight finned tube. The optimum twist ratio and the fin number increase as the pumping power increases.
机译:获得了螺旋翅片管中低雷诺数流量的速度和温度曲线的分析解。螺旋翅片管的单元通道的横截面形状由具有内半径R_I,外半径R_0和顶点角2α的环形扇区描述。通道围绕其纵轴扭曲,扭转长度H.为了简化问题,假设旋转效果可以忽略不计,这对于低雷诺数流动是有效的。通过使用适当的坐标变换,螺旋翅片管中的完全发育的流动可以被视为准二维流动。扰动方法用于解决经受均匀热通量条件的管中的强制对流的变换的动量和能量方程。通过使用用于速度和温度型材的分析解来获得Poiseuille和Nusselt号。以几何参数,2α,r_i = r_i / r_0和w =2πr_0/ h呈现/ re和nu的值。从分析解决方案获得的结果与ω≤0.5和RE <21 /ω的数值结果显示出良好的一致性。这些分析解决方案可用于优化各种约束下螺旋翅片管的热性能。为了说明其有用性,评估了在固定泵送电力的约束下螺旋翅片管的热阻。基于分析溶液,可以分析对给定的非维泵浦功率进行分析确定最小热阻的最佳翅片几何形状。此外,本研究提出了最佳翅片数和最佳捻度比的相关性。根据结果​​,对于相对较低的泵送电源条件(P_(泵)〜*≤P_(泵,断电)〜*)。直翅片管具有比螺旋翅管的热性能更好,随着泵浦功率的增加,最佳翅片数量增加。另一方面,对于相对高的泵送电源条件,(P_(泵)〜*> P_(泵,塞子)〜*),螺旋翅管具有比直翅管的热性能更好。随着泵送功率的增加,最佳捻度和鳍数增加。

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