Low-Reynolds Mathematical Modeling of the Structure of Vortex Zones Between Periodic Surface-Located Flow Turbulators of Semicircular Cross-Section in Pipes

Lobanov Ie
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Abstract

Mathematical modeling of the structure of vortex zones between periodic surface-located flow turbulators of a semicircular and square cross-section is carried out on the basis of multi-block computational technologies based on the solution of the factorized finite-volume method of the Reynolds equations (closed with the help of the Menter shear stress transfer mode) and the energy equation (on different-scale intersecting structured grids). This method was previously successfully applied and verified by experiment. An exhaustive analysis of the corresponding streamlines is presented, proving the advantage of abruded turbulators. A well-known and very well-tested in practice method of vortex intensification of heat transfer is the application of periodic protrusions on the walls of the washed surfaces [1]. The study of the structure of the intensified flow is mainly carried out by experimental methods [1], while modern computational works on this topic are relatively few [2] and are only partially devoted directly to the structure of the intensified flow; some of the methods (for example, a certain part of works [2]) use only integral approaches to this problem. This work is directly devoted to the study of the flow structure in the pipe, For pipes with turbulators of a semicircular cross-section, the nature of the relationship between heat transfer and hydraulic resistance remains similar to the above-considered nature of the relationship for square flow turbulators, but the values (Nu/Nusm)/(  /  sm) for the former, as a rule, is definitely higher due to the much smaller influence of the systems of secondary and corner vortices, which occurs due to deformation and greater elongation of the main vortex, which is confirmed by the corresponding values for pipes with turbulators of a semicircular cross-section (Nu/ Nusm) / (  /  sm)=0.89 t/D
管道半圆截面周期性表面湍流器间涡区结构的低雷诺数数学建模
在求解雷诺方程(借助Menter剪切应力传递模式)和能量方程(在不同尺度相交结构网格上)的分解有限体积法的基础上,基于多分块计算技术,对半圆形和方形截面的周期性表面定位流动器之间的涡区结构进行了数学建模。该方法已成功应用并经实验验证。对相应的流线进行了详尽的分析,证明了磨粒湍流的优点。涡流强化传热的一种众所周知且经过实践检验的方法是在洗涤表面的壁上应用周期性突起[1]。对强化流结构的研究主要是通过实验方法[1]进行的,而现代关于这一主题的计算工作相对较少[2],并且只有部分直接致力于强化流的结构;有些方法(例如,作品[2]的某一部分)只使用积分方法来解决这个问题。这项工作直接致力于研究管流的结构,对管道的紊流器半圆形截面、性质的传热和水力阻力之间的关系仍然是类似于above-considered关系性质广场流紊流器,但值(ν/ Nusm) /(/sm)前,作为一个规则,绝对是由于更高的影响小得多的系统二次涡流和角落,这是由于主涡的变形和较大的伸长引起的,这可以通过带有半圆截面紊流的管道的相应值(Nu/ Nusm) /(/sm)=0.89 t/D
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