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CFD modeling of the atmospheric boundary layer in short test section wind tunnel

机译:短测试区风洞大气边界层的CFD建模

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The aim of this paper is to provide a contribution to algorithms for the numerical simulation of the atmospheric boundary layer (ABL) in short test section wind tunnel, with the lowest pressure loss possible, for large Re, similar to the high values observed in nature. Different turbulent models have been examined for their relative suitability for the atmospheric boundary layer airflow with and without the implementation of buoyancy effects with modified turbulence model constants for the atmosphere. Validation of turbulent models through comparison with wind tunnel experiments is essential for practical applications. It has been observed that the k-ε model is most suitable tool for generation of an ABL in short-chamber wind tunnel. A comparison has been made with the available experimental data, from literature, and the predicted CFD values are very close to the corresponding experimental measurements. The simulation results show the importance of turbulence model constant (C_μ), the non-uniform velocity and turbulence intensity profiles. Also, the significance of y~+ for consistent assessment is confirmed. However, it has been found that the buoyancy force makes significant change in boundary layer thickness without a major impact on computation time.
机译:本文的目的是为在短测试段风洞中进行大气边界层(ABL)数值模拟的算法做出贡献,对于大的Re,压力损失尽可能低,类似于自然界中观察到的高值。已经研究了不同的湍流模型对大气边界层气流的相对适用性,其中带有和不带有浮力效应,并且修改了大气湍流模型常数。通过与风洞实验进行比较来验证湍流模型对于实际应用至关重要。已经观察到,k-ε模型是最适合在短腔风洞中产生ABL的工具。与文献中的可用实验数据进行了比较,预测的CFD值非常接近相应的实验测量值。仿真结果表明了湍流模型常数(C_μ),非均匀速度和湍流强度分布的重要性。同样,确定了y〜+对于一致性评估的重要性。但是,已经发现浮力使边界层厚度发生了显着变化,而对计算时间没有重大影响。

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