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Aerothermal simulation of gas turbine blade cooling channel using Lattice-Boltzmann method
International Journal of Modern Physics C ( IF 1.5 ) Pub Date : 2021-02-25 , DOI: 10.1142/s0129183121500807
Luca Damiola 1 , Maurizio Boffadossi 1 , Lorenzo M. Pii 2 , Alessandro Rossi 2 , Francesco Polidoro 3
Affiliation  

Simulations using the Lattice-Boltzmann Method (LBM) are benchmarked to experimental cooling channel studies performed at the von Karman Institute for Fluid Dynamics. The experimental geometry is representative of a typical rib-turbulated cooling channel for a gas turbine rotor blade. The work aims at describing the flow physics involved, providing a better comprehension of the role of turbulence in augmenting heat transfer. Computations are found to be in agreement with the available experimental data highlighting the accuracy of LBM for aerodynamic and thermal prediction. Results are also compared to Navier–Stokes Large Eddy Simulation (LES). The reduced computational cost compared to LES-based methods offers interesting perspectives for future developments.

中文翻译:

使用格子-玻尔兹曼方法的燃气轮机叶片冷却通道的空气热模拟

使用格子玻尔兹曼方法 (LBM) 的模拟以 von Karman 流体动力学研究所进行的实验冷却通道研究为基准。实验几何结构代表了燃气轮机转子叶片的典型肋湍流冷却通道。这项工作旨在描述所涉及的流动物理学,更好地理解湍流在增强传热中的作用。计算结果与现有的实验数据一致,突出了 LBM 在空气动力学和热预测方面的准确性。结果还与 Navier-Stokes 大涡模拟 (LES) 进行了比较。与基于 LES 的方法相比,降低的计算成本为未来的发展提供了有趣的前景。
更新日期:2021-02-25
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