Numerical simulation of channel flow over a skewed equilateral cavity

IF 0.8 Q2 MATHEMATICS
A. Kamel, E. H. Haraz, S. Hanna
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引用次数: 0

Abstract

In this paper, an incompressible, two-dimensional (2D), time-dependent, Newtonian, laminar, and internal channel fluid flow over a skewed equilateral cavity is simulated using the finite difference method (FDM) and alternating direction implicit (ADI) technique. Navier-Stokes equations are solved numerically in stream function-vorticity formulation. The goal of tackling this problem depends on its academic significance by studying the difference between lid-driven and shear-driven cavity flows in terms of the formation of Moffatt eddies at the sharp corner, also to obtain the length and intensity ratios of these counter-rotating vortices. The value of velocity components along the centerlines of the skewed cavity was revealed at low and intermediate Reynolds numbers (Re), typically (Re = 200 and 2000) at two different skew angles of mainly 30° and 45°. Likewise, the blocked-off regions’ method is used to deal with the geometry of the skewed cavity especially the sharp corners. Furthermore, as Re increases, the main vortex approaches the skewed cavity center and the counter-rotating vortices get bigger in size and intensity, and their number increases. MSC 2010: 76D17, 76D05
倾斜等边空腔沟道流动的数值模拟
本文利用有限差分法(FDM)和交替方向隐式(ADI)技术模拟了一个不可压缩的、二维的、时变的、牛顿的、层流的和内部通道的流体在倾斜等边腔中的流动。采用流函数涡度公式对Navier-Stokes方程进行了数值求解。解决这一问题的目标取决于其学术意义,即研究盖子驱动和剪切驱动的空腔流动在尖角处形成莫法特涡的差异,并获得这些反旋转涡的长度和强度比。在低雷诺数(Re)和中雷诺数(Re = 200和2000)下,以30°和45°两种不同的倾斜角度为主要特征,沿倾斜腔中心线的速度分量值显示。同样地,对于弯曲腔体的几何形状,特别是尖角处,也采用了阻塞区域法。随着Re的增大,主涡向偏斜腔中心靠近,反旋涡的大小和强度增大,反旋涡的数量增加。MSC 2010: 76d17, 76d05
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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来源期刊
CiteScore
2.00
自引率
10.00%
发文量
30
审稿时长
25 weeks
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