Finite Volume Simulation of Newtonian Fluids Through Combined Converging and Diverging Channel

N. Memon, H. Shaikh, B. Shah, A. Baloch
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Abstract

A robust semi-implicit pressure-based Computational Fluid Dynamics (CFD) scheme (SIMPLE) scheme is adopted for modeling of steady and viscous compressible flows through converging and diverging channel. Second-order spatial accuracy will achieved through linear unstructured finite volume cell discretization. The SIMPLE scheme characterizes a development in mass-momentum coupled, pressure based schemes. The governing equations for this scheme are the conservative form of momentum equations (Navier-Stokes) and mass conservation equation. The grid will be developed and refined through Gambit package. Flow structure will be developed with effect of fluid inertia, primary, secondary and treasury vortex may be developed in the aspect ratio 1: 4, 1: 6 and 1: 8 of the converging and diverging channels. The small vortex observed in the ratio 1: 4 in each corner of the channel and with increasing the fluid inertia the left upper vortex in size is enhanced only due to increase the Reynolds numbers. When increased the ratio 1: 6 and 1: 8 the vortex in size is enhanced at lower and upper corner of the channel and occupied the whole domain. Due to filling the Porous material all vortices left, right, upper and lower are diminished and no recirculation flow rate observed at each Reynolds numbers and on every Darcy numbers. The numerical results achieved through finite volume technique through commercial CFD package ANSYS Fluent and will be compared with analytical approach of sheikh, et al. [2012] and also other numerical results with and without use of CFD packages.
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牛顿流体通过收敛和发散联合通道的有限体积模拟
采用一种鲁棒的基于半隐式压力的计算流体动力学(CFD)格式(SIMPLE),对通过收敛和发散通道的定常和粘性可压缩流动进行建模。二阶空间精度将通过线性非结构有限体积单元离散实现。SIMPLE方案的特点是质量动量耦合、基于压力的方案的发展。该方案的控制方程是动量方程的保守形式(Navier-Stokes)和质量守恒方程。网格将通过Gambit包进行开发和完善。在流体惯性的作用下,会形成流动结构,在会聚和发散通道的纵横比为1:4、1:6和1:8时,会形成一次涡、二次涡和库涡。在通道的每个角落观察到1:4比例的小涡,随着流体惯量的增加,左上部涡的大小仅由于雷诺数的增加而增强。当比例分别为1:6和1:8时,涡的大小在通道的上下角增强,并占据整个区域。由于填充了多孔材料,左、右、上、下的所有涡旋都减弱了,在每个雷诺数和每个达西数上都没有观察到再循环流量。将有限体积技术通过商用CFD软件包ANSYS Fluent获得的数值结果与sheikh等[2012]的分析方法以及使用和不使用CFD软件包的其他数值结果进行比较。
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