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Non-Newtonian fluid flow around a Y-shaped fin embedded in a square cavity

机译:非牛顿流体流动在嵌入方形腔内的Y形翅片周围流动

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This study investigates the free convection of Casson fluid inside a square cavity with intruded Y-shaped fin at the bottom surface. The Casson fluid is a non-Newtonian fluid and has an infinite viscosity at zero rates of shear. This is the first time that this fluid is used in the square cavity containing Y-shaped fin at the bottom surface. The Y-shaped fin helps in understanding the constructal theory and enhancing the heat transfer rate from the fin. The main objective of using this fin is to increase the convective heat transfer surface area. The sidewalls of the cavity are kept at cold temperature, the bottom surface at a hot temperature, and the top surface as adiabatic. The tips of the Y-shaped fin are considered as hot, cold, and adiabatic. The effects of the magnetic field and radiation are included in the momentum and energy equations. The influence of viscous heating is neglected. The buoyancy term is included in the momentum equation using Boussinesq approximation. The dimensionless governing equations are solved numerically using a Galerkin weighted residual technique of the finite element method. The effects of Rayleigh number (Ra = 10(4)-10(6)), radiation parameter (R-d = 0-10(3)), Hartmann number (Ha = 0-10(3)), and Casson parameter (gamma = 0.1-1) on streamlines, isotherms, dimensionless velocity components, temperature, and local Nusselt numbers along the fin and the bottom heated wall are investigated and presented graphically. It is demonstrated that, in the presence of Y-shaped fin, all the pertinent parameters and dimensionless numbers help in enhancing the heat transfer rate along the bottom surface.
机译:本文研究了卡森流体在底部有Y形翅片的方形空腔内的自由对流。卡森流体是一种非牛顿流体,在零剪切速率下具有无限粘性。这是该流体首次用于底部表面含有Y形翅片的方形腔体中。Y形翅片有助于理解结构理论,提高翅片的传热率。使用这种翅片的主要目的是增加对流传热表面积。空腔的侧壁保持低温,底面保持高温,顶面保持绝热。Y形翅片的尖端被认为是热的、冷的和绝热的。磁场和辐射的影响包含在动量和能量方程中。粘性加热的影响被忽略。使用Boussinesq近似将浮力项包含在动量方程中。采用有限元法中的伽辽金加权残数法数值求解无量纲控制方程。研究了瑞利数(Ra=10(4)-10(6))、辐射参数(R-d=0-10(3))、哈特曼数(Ha=0-10(3))和卡森参数(gamma=0.1-1)对翅片和底部加热壁流线、等温线、无量纲速度分量、温度和局部努塞尔数的影响,并用图形表示。结果表明,在Y形翅片的存在下,所有相关参数和无量纲数都有助于提高沿底面的传热速率。

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