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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:压缩偏移湍流喷射撞击平坦表面的空气动力学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:在本文中,对撞击平坦表面的限制偏移湍流平面射流的传热特性。特别兴趣的参数是喷射偏移距离和喷射出口温度。喷射出口温度在100〜0℃下保持恒定,而在23〜0℃下板温度均匀。对于所提述的喷射温度,用喷射出口宽度归一化的偏移距离从0.5(壁射流)变化为4.对于所有情况下,喷射出口雷诺数为4000.使用商业软件ANSYS流畅的灭火射流的产生气体动力学特性及其随后的传热行为。鉴定了产生最大传热的构造。一旦墙壁喷射开发,超出了停滞点下游的一定距离,速度和温度曲线显示了相似性行为。已经讨论了2-D和3-D案件的结果。在撞击之后跟踪速度和热边界层,与简单的平板相比。可以基于速度趋势来预测热行为。

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