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Laminar Wall Jet Flow and Heat Transfer over a Shallow Cavity

机译:层壁射流流动和传热在浅腔内

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摘要

This paper presents the detailed simulation of two-dimensional incompressible laminar wall jet flow over a shallow cavity. The flow characteristics of wall jet with respect to aspect ratio (AR), step length (Xu), and Reynolds number (Re) of the shallow cavity are expressed. For higher accuracy, third-order discretization is applied for momentum equation which is solved using QUICK scheme with SIMPLE algorithm for pressure-velocity coupling. Low Reynolds numbers 25, 50, 100, 200, 400, and 600 are assigned for simulation. Results are presented for streamline contour, velocity contour, and vorticity formation at wall and also velocity profiles are reported. The detailed study of vortex formation on shallow cavity region is presented for various AR,Xu, and Re conditions which led to key findings as Re increases and vortex formation moves from leading edge to trailing edge of the wall. Distance between vortices increases when the step length (Xu) increases. When Re increases, the maximum temperature contour distributions take place in shallow cavity region and highest convection heat transfer is obtained in heated walls. The finite volume code (FLUENT) is used for solving Navier-Stokes equations and GAMBIT for modeling and meshing.
机译:本文介绍了浅腔内二维不可压缩层壁射流的详细仿真。表达了浅腔的纵横比(AR),步长(Xu)和雷诺数(Re)的壁射流的流动特性。为了更高的精度,使用具有快速方案的动量方程来应用三阶离散化,以简单的压力 - 速度耦合算法解决。为模拟分配低雷诺数25,50,100,20,400和600。结果以墙壁的速度轮廓,速度轮廓,速度形成以及速度形成的结果。对于各种AR,XU和RE条件,给出了浅腔区域上的涡流形成的详细研究,其作为重新增加和涡流形成从墙壁的前缘移动到墙壁上的关键发现。当步长(XU)增加时涡流之间的距离增加。当重新增加时,在浅腔区域中发生最大温度轮廓分布,并且在加热的壁中获得最高的对流传热。有限卷代码(流利)用于解决Navier-Stokes方程和Gambit以进行建模和啮合。

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