Theory of Heat Transfer in Straight Round Pipes with Square and Triangular Turbulators Under High Reynolds Criteria

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Abstract

Objectives: To carry out mathematical modeling of the structure of vortex zones between periodic flow turbulators with a surface arrangement of triangular and square transverse profiles on the basis of multi-block computing technologies based on solutions of the Reynolds equations (closed by means of the Menter shear stress transfer model) and energy equations (on multi-scale intersecting structured grids) with high Reynolds criteria Re = 106 with an exhaustive analysis of the corresponding current lines. Method: The calculations were carried out on the basis of a theoretical method based on the solution of the Reynolds equations by the factorized finite-volume method, which are closed using the low-Reynolds model of the Menter shear stress transfer, and the energy equation on multi -scale intersecting structured grids (FCOM). Result: Mathematical simulations of the heat exchange process in straight and round pipes with turbulators with d / D = 0.95 ... 0.90 and t / D = 0.25 ... 1.00 square and triangular cross-sections at large Reynolds numbers (Re = 106) on a foundation with multi-block computing technologies, which are based on solutions of the Reynolds equations and energy equations in a finite-volume and factorized way. It is found that the relative intensification of heat transfer [(Nu / Nusm) | Re = 106] / [(Nu / Nusm) | Re = 105] in round pipes with square air turbulators for large Reynolds numbers (Re = 106), which may well be relevant in the channels used in heat exchangers, may be higher with a large-scale increment of hydraulic resistance than for slightly smaller numbers (Re = 105), for relatively high flow turbulators d / D = 0. 90 for the entire range under consideration for the parameter of the relative step between them t / D = 0.25 ... 1.00 a little more than 3%; for turbulators of triangular cross-section, similar indicators are approximately the same. For lower square turbulators with d / D = 0.95, this increase in relative heat transfer for large Reynolds numbers (Re = 106) compared to smaller numbers (Re = 105) does not exceed 6%; for triangular cross-section turbulators, similar indicators are slightly more than 4%. Conclusion: According to the results of calculations based on the developed model, it is possible to optimize the intensification of double turbulators, as well as to control the process of heat transfer intensification. It is shown that for higher square turbulators and at higher Reynolds numbers, a slight increase in the relative Nusselt number Nu / Nusm is accompanied by a significant increase in the relative hydraulic resistance due to the very significant influence of return currents, which can flow directly on the turbulator itself to the greater extent, the higher the Reynolds number; for triangular turbulators, the above trend persists and even deepens.
高雷诺数条件下带有方形和三角形湍流体的直圆管内换热理论
目的:基于高雷诺数准则Re = 106的雷诺方程(用Menter剪切应力传递模型封闭)和能量方程(在多尺度相交结构网格上)的解,并对相应的电流线进行详尽分析,基于多块计算技术,对三角形和方形横剖面表面布置的周期流紊流之间的涡区结构进行数学建模。方法:基于基于分解有限体积法求解雷诺方程的理论方法进行计算,该方法采用Menter剪切应力传递的低雷诺数模型和多尺度相交结构网格(FCOM)上的能量方程进行封闭。结果:在d / d = 0.95的条件下,用数学方法模拟了带紊流器的直管内和圆管内的换热过程。0.90, t / D = 0.25…基于基于有限体积分解的雷诺方程和能量方程解的多块计算技术,在大雷诺数(Re = 106)下的1.00个正方形和三角形截面。发现的相对强化传热((ν/ Nusm) | Re = 106] /[(ν/ Nusm) | Re = 105]在圆形管道与方形空气湍流器大雷诺数(Re = 106),这可能是有关在热交换器中使用的通道,可能更高的大规模增加液压阻力比略小的数字(Re = 105),相对较高的流紊流器d / d = 0。对于它们之间的相对步长参数t / D = 0.25…1.00略高于3%;对于三角形截面的紊流,类似的指标大致相同。对于d / d = 0.95的较低方形紊流,与较小雷诺数(Re = 105)相比,大雷诺数(Re = 106)的相对传热增加不超过6%;对于三角形截面的紊流,类似指标略大于4%。结论:根据所建立模型的计算结果,可以优化双紊流强化,并控制传热强化过程。结果表明,对于较大的方形湍流,在较高的雷诺数下,由于回流的影响非常显著,相对努塞尔数Nu / Nusm的轻微增加伴随着相对水力阻力的显著增加,回流对湍流本身的直接作用程度越大,雷诺数越高;对于三角形湍流,上述趋势持续甚至加深。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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