Heat Transfer Enhancement by Turbulent Impinging Jets

M. Kumagai, R. Amano, M. Jensen
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Abstract

A numerical and experimental investigation on cooling of a solid surface was performed by studying the behavior of an impinging jet onto a fixed flat target. The local heat transfer coefficient distributions on a plate with a constant heat flux were computationally investigated with a normally impinging axisymmetric jet for nozzle diameter of 4.6mm at H/d = 4 and 10, with the Reynolds numbers of 10,000 and 40,000. The two-dimensional cylindrical Navier-Stokes equations were solved using a two-equation k-ε turbulence model. The finite-volume differencing scheme was used to solve the thermal and flow fields. The predicted heat transfer coefficients were compared with experimental measurements. A universal function based on the wave equation was developed and applied to the heat transfer model to improve calculated local heat transfer coefficients for short nozzle-to-plate distance (H/d = 4). The differences between H/d = 4 and 10 due to the correlation among heat transfer coefficient, kinetic energy and pressure were investigated for the impingement region. Predictions by the present model show good agreement with the experimental data.
紊流冲击射流增强传热
通过研究射流对固定平面目标的冲击行为,对固体表面的冷却进行了数值和实验研究。研究了在H/d = 4和10、雷诺数为10000和40000时,喷嘴直径为4.6mm的正碰撞轴对称射流在恒热流密度条件下的局部换热系数分布。采用两方程k-ε湍流模型求解二维圆柱形Navier-Stokes方程。采用有限体积差分格式求解热场和流场。将预测的换热系数与实验值进行了比较。建立了基于波动方程的通用函数,并将其应用于传热模型中,以改进喷嘴到板距离较短(H/d = 4)时计算的局部换热系数。研究了撞击区域换热系数、动能和压力之间的相关性对H/d = 4和10之间的差异。该模型的预测结果与实验数据吻合较好。
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