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NUMERICAL ANALYSIS OF LOCAL HEAT TRANSFER FROM A FLAT PLATE TO A SWIRLING AIR IMPINGING JET

机译:从平板到旋转空气撞击射流的局部传热的数值分析

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Local heat transfer from a flat plate to a swirling circular air impinging jet is investigated numerically. Reynolds Averaged Navier-Stokes equations (RANS) and energy equation are solved for the axisymmetric, three dimensional flow. Eddy-viscosity based turbulence models, RNG and V2F, are used. Non-uniform meshes are used for the three dimensional flows and mesh independent solutions are obtained. The flow Reynolds number, which is based on the jet diameter, is kept at 23,000. In the analysis, local heat transfer coefficients are obtained for different swirl numbers, S = 0.21, 0.35 and 0.47 and jet-to-plate distance, L/D, ranging from 2 to 9. Investigation of the effect of swirl flow profile at the exiting plane of the jet on heat transfer is also presented. It is found that different swirl profiles with the same swirl number lead to very different heat transfer behaviors in the stagnation region of the impinging jet.
机译:在数值上研究了从平板到旋流圆形空气撞击射流的局部热传递。 Reynolds平均Navier-Stokes方程(RANS)和能量方程被求助于轴对称,三维流动。 基于涡流粘度的湍流模型,RNG和V2F。 非均匀网格用于三维流动,获得网状独立解决方案。 基于喷射直径的流动雷诺数保持在23,000。 在分析中,获得不同涡流数的局部传热系数,S = 0.21,0.35和0.47和喷射板距离,L / D,范围为2至9.调查旋流流动曲线在的效果 还提出了在热传递上出口喷射的平面。 发现具有相同旋流数的不同涡流谱引入撞击射流的停滞区域中的非常不同的传热行为。

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