标题: 利用叶片式涡流产生器之热传增强
Heat Transfer Enhancement by Myltilobe Vortex Generators
作者: 吕宪伟
Leu, Shiann-Woei
崔燕勇
Tsui Yeng-Yung
机械工程学系
关键字: 叶片式涡流产生器;热传
公开日期: 1996
摘要: 本论文是以数值方法研究在圆管流内入叶片式涡流产生器的流场
与热传增强效果。统御方程式转换至非正交曲线座标上,利用有限体
积积分法将方程式离散化,压力之离散化采用相邻19点相关格点求解,
计算格点则使用非交错式纲格布置,再以SIMPLE法则求解代数方程式。
研究范围包括:一.雷诺数为以2000基准,Prandtl numbre为5,内置
各种不同型式涡流产生器之光滑管流场及热传分析;二.在上述圆管
内附加不同长度鳍片,分析其热传增强效果;三.对光滑管之紊流流
场进行数值分析。
叶片式涡流产生器可以诱导出次级速度,并在叶片出口后短距离
内形成轴向涡流,轴向涡流可以导致热传的增强,然而壁面的磨擦及
压降的损失亦增大。增加叶片之轴向斜率对于热传的增强有很大的帮
助,例如增加叶片的高度、减少叶片的轴向长度及使用向内凹的叶片
形状皆可增加热传,此外,叶片数采用五或六片的涡流产生器有较佳
的性能。对于A型叶片式涡流产生器圆管流,增加鳍片有助于热传增强,
且鳍片的长度越大,热传量越大。对于A型叶片式涡流产生器完成雷
诺数2×105紊流范围之流场与热传数值分析。其热传量、环流量及摩
擦系数皆较层流者大为增加。
The flow and heat transfer in a tube with multilobe vortex generators inserted are studied using numerical method. The governing equations are transferred to curvilinear coordinates to fit the irregular geometry. Discretization is made by using the finite-volume integral method with non-staggered grid arrangement. The pressure-correction equation is solved over 19 neighboring points. The system of algebra equations are solved by the SIMPLE-type algorithm. Categories of the thesis have three departments: 1. Analysis a tube flow by putting multilobe vortex generator in it. The Reynolds number is mainly fixed at 2000 and the Prandtl number is 5. 2: inside the wall of the above-mentioned tube, we added different length of fins, to analysis the heat enhancement 3: Analysis of the turbulent flow of the smooth tube.
When fluid flows through the vortex generator, secondary velocities are induced and axial vortices are formed after a short distance downstream of the exist of the lobe. The axial vortices leads to enhancement of heat transfer as well as friction and pressure loss.. Heat transfer can be improved by increasing the axial slope of the lobe through increasing the lobe penetration, reducing the lobe length, and making a concave lobe shape. Five or six lobes for the vortex generator are sufficient to y ield good performance. The heat transfer can be improved by increasing the length of fins. A three-dimensional flow calculation procedure has been successfully incorporated to study the turbulent flow for Reynolds number is 2×105. It's heat transfer, circulation and friction coefficient is much larger than laminar flow.
URI: http://140.113.39.130/cdrfb3/record/nctu/#NT853489029
http://hdl.handle.net/11536/62377
显示于类别:Thesis