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Computational Investigation of Aerodynamic and Heat Transfer Characteristics of a Confined Offset Turbulent Jet Impinging on a Flat Surface

机译:撞击在平坦表面上的受限偏置湍流射流的空气动力和传热特性的计算研究

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The heat transfer characteristics of a confined offset turbulent plane jet impinging a flat surface is investigated numerically in this paper. The parameters of particular interest are the jet offset distance and jet exit temperature. The jet exit temperature was held constant at 100~0 C while the plate temperature was uniform at 23~0 C. For the mentioned jet temperature, the offset distance normalized with jet exit width is varied from 0.5 (wall jet) to 4. For all cases, the jet exit Reynolds number was 4000. The resulting aerodynamic characteristics of the impinging jet and its consequent heat transfer behavior were studied using the commercial software ANSYS FLUENT. The configuration which yielded the maximum heat transfer was identified. Once the wall jet developed, beyond a certain distance downstream of the stagnation point, the velocity and temperature profiles displayed similarity behavior. Results for the 2-D and 3-D cases have been discussed. The velocity and thermal boundary layers were tracked following impingement and compared to that of a simple flat plate. The thermal behavior could be predicted based on the velocity trends.
机译:数值研究了有限的偏心湍流平面射流撞击平面的传热特性。特别感兴趣的参数是射流偏移距离和射流出口温度。射流出口温度保持恒定在100°C至0°C,而板温度在23°C至0°C均匀。对于上述射流温度,通过射流出口宽度归一化的偏移距离从0.5(壁射流)变为4。在所有情况下,射流出口的雷诺数为4000。使用商业软件ANSYS FLUENT研究了撞击射流的空气动力学特性及其随后的传热行为。确定了产生最大热传递的构型。一旦壁流形成,在停滞点下游一定距离之外,速度和温度分布显示出相似的行为。讨论了2-D和3-D情况的结果。撞击后追踪速度和热边界层,并与简单平板的速度和热边界层进行比较。可以基于速度趋势预测热行为。

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