Numerical analysis of the heat transfer on tandem cylinders, inline and staggered geometries in cross flow of air are investigated for different geometry and flow conditions. finite element method is sued to solve Navier-Stokes and energy equations. Local variations are presented for tandem cylinders geometry with L/ D=1.13, 2,3,6 and Reynolds number is fixed as 400. Three isothermal cylinders for Staggered geometry, four isothermal cylinders for inline geometry were placed in a Wide channel and S_r x S_1 was fixed as 2x2 and Reynolds number was varied as the Value of 80, 120, 200.
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机译:针对不同的几何形状和流动条件,对串联气缸,直列和交错几何形状在空气交叉流动中的传热进行了数值分析。采用有限元方法求解Navier-Stokes方程和能量方程。提出了L / D = 1.13、2、3、6和雷诺数固定为400的串联圆柱几何体的局部变化。将三个交错几何体的等温圆柱体,四个串联几何体的等温圆柱体放置在宽通道中,S_r x S_1固定为2x2,雷诺数随着值80、120、200而变化。
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