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首页> 外文期刊>Case Studies in Thermal Engineering >Heat transfer analysis on buoyantly convective non-Newtonian stream in a hexagonal enclosure rooted with T-Shaped flipper: Hybrid meshed analysis
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Heat transfer analysis on buoyantly convective non-Newtonian stream in a hexagonal enclosure rooted with T-Shaped flipper: Hybrid meshed analysis

机译:六角形外壳中浮相对流非牛顿流的传热分析,含有T形鳍状公司的旋转型鳍状公司:杂交网状分析

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It is well consensus among researchers that the non-Newtonian fluid equipped in closed enclosures brings complicated mathematical models and hence one cannot examine flow field truly. The present attempt is first numerical investigation to evaluate the buoyantly convective non-Newtonian fluid flow equipped in hexagonal shaped cavity. The uniformly heated T-shaped fin is embedded at lower wall of hexagonal cavity. The top wall of hexagonal cavity is manifested with an adiabatic condition. The bottom wall of enclosure is taken uniformly heated. Both left and right walls are kept cold. The buoyantly convective Casson fluid flow around uniformly heated T-shaped fin is mathematically controlled by way of system of partial differential equations. The finite element method is adopted to report numerical solution. The hexagonal enclosure as a computational domain is discretized by means of both triangular and rectangular elements. The velocity and temperature distribution around uniformly heated T-shaped are examined towards Rayleigh number. The line graph study is also executed to report the dimensionless Casson fluid and Casson temperature along center and vertical line directions of T-shaped fin. The impact of Rayleigh number on heat transfer rate along the surface of heated fin is also examined and offered by means of line graph. It is observed that the heat transfer rate enhances along the surface of T-shaped fin when we increase the Rayleigh number.
机译:在封闭式外壳中的非牛顿流体之间的研究人员之间是良好的共识,使复杂的数学模型带来了复杂的数学模型,因此无法真正检查流场。目前的尝试是评估配备在六边形腔中的浮标的对流非牛顿流体流动的重要数值调查。均匀加热的T形翅片嵌入六边形腔的下壁上。六边形腔的顶壁表现为绝热条件。外壳的底壁均匀加热。左右墙都保持冷。通过部分微分方程的系统在数学控制周围均匀地加热的T形翅片的浮动对流腺体流体。采用有限元方法报告数值解。作为计算域的六边形机箱通过三角形和矩形元件离散化。均匀加热的T形周围的速度和温度分布被检查为瑞利数。还执行线图研究以报告无量纲的腺体流体和沿T形鳍片的中心和垂直线方向的烧调茶温度。还通过线图检查和提供了沿着加热翅片表面的瑞利数对热传递速率的影响。观察到,当我们增加瑞利数时,传热速率沿着T形鳍片的表面增强。

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