层流区带粘性热载体紊流的管道内流动和换热的模拟,以及向紊流过渡的模拟

I. E. Lobanov
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引用次数: 0

摘要

目标。利用该计算方法,建立了具有层流流态和瞬态流态特征的粘性热载体管内紊流传热的数学模型。基于因式有限体积法(FCOM)求解雷诺方程(在瞬态模式下采用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),考虑了基于多块计算技术的半圆截面流紊流换热问题的求解。方法。计算采用基于Reynolds方程解的理论方法,瞬态模式下采用Menter剪切应力传递模型,多尺度相交结构网格(FCOM)上的能量方程采用因式有限体积法进行计算。结果。本文利用FCOM方法得到了一种黏性冷却剂层流和瞬态流动模式下管内流动和换热的局部和平均特性,从而可以确定这些模式下的换热强化水平与已有的实验结果相吻合。结论。低高度紊流相对水阻力计算值增加幅度较小,中高度紊流相对水阻力计算值达到临界雷诺数2÷2.5,随后增加幅度可达3倍;对于高紊流,在达到过渡流型之前,相对水力阻力增加了4倍,过渡流型之后,相对水力阻力增加了4.5倍。相对高紊流在粘性冷却剂层流状态下的相对等温强化换热计算结果增加了近2倍;对于相对中等高度的紊流-几乎是一个半,以及相对较低的高度,热交换的强化是微不足道的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Modeling of the flow and heat exchange in pipes with turbulators of viscous heat carriers in the laminar region, as well as in the transition to turbulent flow
Objective . Mathematical modeling of heat transfer in pipes with turbulators for viscous heat carriers at Reynolds numbers characteristic of laminar and transient flow regimes is carried out by the calculation method. The solution of the heat exchange problem for semicircular cross-section flow turbulators based on multiblock computing technologies based on the solution of the Reynolds equations (closed for the transient mode using the Menter shear stress transfer model) and the energy equation (on multi-scale intersecting structured grids) by the factorized finite-volume method (FCOM) was considered. Method . The calculation was carried out on the basis of a theoretical method based on the solution of the Reynolds equations, closed for transient modes using the Menter shear stress transfer model, and the energy equation on multiscale intersecting structured grids (FCOM), by a factorized finite-volume method. Result . Both local and averaged characteristics of the flow and heat exchange in pipes with turbulators for a viscous coolant for laminar and transient flow modes of the coolant were obtained using the FCOM method in the work, which made it possible to determine for these modes the levels of heat exchange intensification that satisfactorily correlate with the existing experiment. Conclusion . The calculated relative hydraulic resistance for low turbulators increases quite slightly, and for medium-altitude turbulators reaches 2÷2.5 to the critical Reynolds number, and subsequently it increases up to 3 times; for high turbulators, the relative hydraulic resistance increases up to 4 times even before the transition flow regime is reached, after which it increases up to 4.5 times. The calculated relative isothermal intensified heat exchange under the laminar flow regime of a viscous coolant for relatively high turbulators increases almost 2 times; for relatively medium heights of turbulators — almost one and a half, and for low relative heights, the intensification of heat exchange is insignificant.
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