Asymptotic and numerical solutions of three-dimensional boundary-layer flow past a moving wedge

被引:8
|
作者
Kudenatti, Ramesh B. [1 ]
Gogate S, Shashi Prabha [1 ]
Bujurke, N. M. [2 ]
机构
[1] Bangalore Univ, Dept Math, Cent Coll Campus, Bangalore 560001, Karnataka, India
[2] Karnatak Univ, Dept Math, Dharwad 580003, Karnataka, India
关键词
3-dimensional boundary-layer; asymptotics; displacement thickness; Keller box; similarity transformations; wedge flow; POINT; NANOFLUID;
D O I
10.1002/mma.4761
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
We consider a laminar boundary-layer flow of a viscous and incompressible fluid past a moving wedge in which the wedge is moving either in the direction of the mainstream flow or opposite to it. The mainstream flows outside the boundary layer are approximated by a power of the distance from the leading boundary layer. The variable pressure gradient is imposed on the boundary layer so that the system admits similarity solutions. The model is described using 3-dimensional boundary-layer equations that contains 2 physical parameters: pressure gradient () and shear-to-strain-rate ratio parameter (). Two methods are used: a linear asymptotic analysis in the neighborhood of the edge of the boundary layer and the Keller-box numerical method for the full nonlinear system. The results show that the flow field is divided into near-field region (mainly dominated by viscous forces) and far-field region (mainstream flows); the velocity profiles form through an interaction between 2 regions. Also, all simulations show that the subsequent dynamics involving overshoot and undershoot of the solutions for varying parameter characterizing 3-dimensional flows. The pressure gradient (favorable) has a tendency of decreasing the boundary-layer thickness in which the velocity profiles are benign. The wall shear stresses increase unboundedly for increasing when the wedge is moving in the x-direction, while the case is different when it is moving in the y-direction. Further, both analysis show that 3-dimensional boundary-layer solutions exist in the range -1<<. These are some interesting results linked to an important class of boundary-layer flows.
引用
收藏
页码:2602 / 2614
页数:13
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