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Numerical simulation of turbulent boundary layers with foreign gas transpiration using OpenFOAM

机译:利用OpenFOAM进行异物蒸发的湍流边界层的数值模拟。

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摘要

Transpiration cooling in combination with porous high-temperature materials is a promising technique for thermal protection of highly-loaded aerospace applications. In this study, we present a modified OpenFOAM solver which is applied to the simulation of a turbulent channel flow with boundary layer blowing. Different models for porous wall injection of air, argon, and helium into a main flow of air are proposed and evaluated. Subsequently, same and foreign gas transpiration is simulated for cold and heated main flow conditions and the results are compared to experimental data and correlations from literature. A very good overall agreement is found for velocity and temperature boundary layer profiles as well as the dimensionless parameters for wall shear stress and heat transfer.
机译:蒸腾冷却与多孔高温材料相结合是一种用于高负荷航空航天应用的热保护技术。在这项研究中,我们提出了一种改进的OpenFOAM求解器,该求解器用于模拟边界层吹动的湍流通道。提出并评估了用于将空气,氩气和氦气注入空气主流中的多孔壁的不同模型。随后,对冷,热主流条件下的相同和外来气体蒸发进行了模拟,并将结果与​​实验数据和文献的相关性进行了比较。对于速度和温度边界层轮廓以及壁面剪应力和热传递的无量纲参数,发现了一个非常好的总体协议。

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