THE SIMULATION AND FEATURES OF COUNTERCURRENT FLOW IN VERTICAL CHANNELS OF CONTACT DEVICES

I. Kuzmenko
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Abstract

The aim of the work is to study the modes of motion of the phases at the interface of the film of water-air flow in the vertical channel during the countercurrent motion of the phases of the coolant. To achieve this goal, the following problems are solved: for each of the phases, the stationary Navier-Stokes equations and continuity are recorded, taking into account the direction of gravity. The obtained system of equations in the two-dimensional formulation in cylindrical coordinates with corresponding boundary conditions is solved in the package COMSOL MULTIPHYSICS 5.6. In the specified package the modeling of the influence of factors on the behavior of the interface of the film water-air flow in the vertical channel during the countercurrent movement of the phases is carried out. It is concluded that the existence of concomitant flows at the interface of the phases, depending on the height of the channel and the flow of phases in the vertical channel. As a result of the simulation, it was found that the countercurrent phases in the laminar mode in the vertical channel, the hydrodynamics at the interface of the phases differs in the height of the channel. At the inlet, at the bottom of the channel, the airflow creates a concomitant flow in the flowing film of water at the interface. Accordingly, at the top of the channel, at the inlet, the film of water creates a concomitant flow in the flow of wind, moving countercurrent. And in the canal itself, there is an area where the movement of water and air flows has no concomitant flows. That is, as a result of simulation it was found that the countercurrent phases in the laminar mode in the vertical channel, the hydrodynamics at the phase boundary differs, depending on the zone at the height of the channel and three such zones. Factors that affect the size of the above three zones are the height of the channel, flow rate, or speed of each of the phases. In particular, at the inlet of the water film into the channel with a speed  = 0,3…1,1 m/s and a thickness of 0.25 mm (= 60… 210), the calculated value of the thickness of the concomitant airflow is (0.4 .. 1.6) 103 m and is directly proportional to the speed of the water film. Also, with a decrease in the height of the canal three times, from 0.150 to 0.050 m, the existence of three zones in the canal is maintained, but the height of the zone without concomitant flow decreases in direct proportion by one order - from 0.137 m to 0.0113 m. The establishment of co-directed flows at the phase separation boundary in the channels of film contact devices for selection of the hydrodynamic regime to increase the efficiency of heat exchange.
接触装置垂直通道逆流的模拟与特性研究
本文的目的是研究在冷却剂相的逆流运动过程中,垂直通道中水气膜界面处相的运动模式。为了实现这一目标,解决了以下问题:对于每个相,考虑重力方向,记录稳态Navier-Stokes方程和连续性。在COMSOL MULTIPHYSICS 5.6软件包中求解了具有相应边界条件的柱坐标二维方程组。在指定的包中,进行了在相的逆流运动过程中,各因素对垂直通道中膜水-气流动界面行为的影响的建模。结果表明,在两相界面处是否存在共流,取决于通道的高度和垂直通道内的相流。模拟结果表明,在垂直通道中存在层流模式的逆流相,两相界面处的水动力随通道高度的不同而不同。在入口,在通道的底部,气流在界面处的水流动膜中产生伴随流。相应地,在通道的顶部,在入口处,水膜在风的流动中产生了伴随流,移动逆流。在运河本身,有一个区域,水和空气的流动没有伴随的流动。也就是说,通过模拟发现,垂直通道中层流模式的逆流相,相边界处的流体力学是不同的,这取决于通道高度的区域和三个这样的区域。影响上述三个区域大小的因素是通道的高度、流速或每一相的速度。特别是在进入通道的水膜入口以速度= 0,3…1,1 m/s,厚度为0.25 mm(= 60…210)时,伴随气流厚度的计算值为(0.4…1.6) 103 m,与水膜的速度成正比。同时,随着运河高度从0.150 m下降到0.050 m的三倍,运河内保持了三个区域的存在,而无伴随流区域的高度则成正比地下降了一个数量级,从0.137 m下降到0.0113 m。在膜接触装置通道的相分离边界处建立共向流动,选择流体动力形式,提高换热效率。
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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