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Direct numerical simulation of heat transfer in a spatially developing turbulent boundary layer

机译:在空间发展的湍流边界层中传热的直接数值模拟

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Direct numerical simulation has been performed to investigate heat transfer in a zero-pressure-gradient spatially developing turbulent boundary layer with realistic thermal inflow boundary conditions. The temperature is considered as a passive scalar and the molecular Prandtl number is set to be 0.71. The turbulence statistics for both the velocity and temperature fields show good agreement with previous numerical and experimental data in the literature. The present study provides a valuable database for the spatially developing turbulent thermal boundary layer over a wide range of Reynolds numbers from Re-theta = 1100 to 1940. The simulation results indicate that both the peak value and peak location of the streamwise velocity fluctuation grow slightly with increasing Reynolds number, same as those of the temperature fluctuation. The relationship between the streamwise velocity and temperature fluctuations has been examined and a strong correlation is observed in the vicinity of the wall. With increasing distance from the wall, however, the degree of correlation significantly decreases. In addition, the difference between the turbulent velocity and temperature fields is also analysed by investigating the mechanisms of heat and momentum transport in boundary layer flow. Published by AIP Publishing.
机译:已经进行了直接数值模拟,以研究具有实际热流入边界条件的零压力梯度空间发展湍流边界层中的传热。温度被认为是被动标量,分子的Prandtl数设为0.71。速度场和温度场的湍流统计数据与文献中先前的数值和实验数据显示出良好的一致性。本研究为从Re-theta = 1100到1940的宽范围的雷诺数在空间上发展的湍流热边界层提供了有价值的数据库。模拟结果表明,沿流速度波动的峰值和峰值位置都略有增长随着雷诺数的增加,与温度波动相同。已经检查了气流速度和温度波动之间的关系,并且在壁附近观察到很强的相关性。但是,随着距墙壁的距离增加,相关程度显着降低。此外,还通过研究边界层流中的热和动量传输机制来分析湍流速度和温度场之间的差异。由AIP Publishing发布。

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