Usage of high-fidelity large eddy simulation to improve the turbulence modeling of Reynolds averaged navier stokes simulation in film cooling applications via a neural network

被引:0
作者
Mazaheri K. [1 ]
Abtahi Mehrjardi S.A. [1 ]
机构
[1] Department of Aerospace Engineering, Sharif University of Technology, Tehran
关键词
Film cooling; Large eddy simulation; Neural network; Surrogate modeling; Turbulence modeling; Turbulent prandtl number;
D O I
10.1016/j.ijft.2024.100718
中图分类号
学科分类号
摘要
In this study, high-Fidelity Large eddy simulation (LES) data was used to create a surrogate turbulence model to enhance the estimation of turbulent heat flux in a Reynolds averaged Navier Stokes (RANS) solver for film cooling applications. The LES simulation (A flat plate film cooling application with a Reynolds number of 17,382, a blowing ratio of 1 and a density ratio of 2) was validated by comparison with experimental data. A correlation analysis was performed to identify the most influential parameters, and temperature gradient, velocity gradient, turbulent dissipation rate, shear strain rate, and turbulent viscosity ratio were selected as the most effective parameters. A second model was developed to create a Galilean-invariant model that remains unaffected by changes in the coordinate system. Neural network was applied to the LES training data to propose a modified surrogate dynamic turbulent Prandtl number to be applied to the k − ε realizable RANS simulation. The first surrogate model was implemented to two different geometries, one geometry was a flat plate film cooling similar to the training data but with different flow conditions, and another one was a more complex geometry with pressure gradient. The second model was only implemented on the second geometry and produced similar results. The surrogate models predicted a more accurate thermal field near the cooling wall (up-to 58 % error reduction) with a computational time complexity similar to the base RANS solver. © 2024 The Author(s)
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共 55 条
[1]  
Zamiri A., You S.J., Chung J.T., Large eddy simulation of unsteady turbulent flow structures and film-cooling effectiveness in a laidback fan-shaped hole, Aerosp. Sci. Technol., 100, (2020)
[2]  
Kim C., Son C., Rapid design approach for U-bend of a turbine serpentine cooling passage, Aerosp. Sci. Technol., 92, pp. 417-428, (2019)
[3]  
Yang B., Et al., Evaluation of variable rotation on enhancing thermal performance of phase change heat storage tank, Int. J. Heat Fluid Flow, 106, (2024)
[4]  
Peterson S., Plesniak M., Evolution of jets emanating from short holes into crossflow, J. Fluid Mech., 503, pp. 57-91, (2004)
[5]  
Jovanovic M., De Lange H., Van Steenhoven A., Influence of hole imperfection on jet cross flow interaction, Int. J. Heat Fluid Flow, 27, 1, pp. 42-53, (2006)
[6]  
Varol Y., Et al., Experimental study and Large Eddy Simulation of thermal mixing phenomena of a parallel jet with perforated obstacles, Int. J. Therm. Sci., 111, pp. 1-17, (2017)
[7]  
Bernsdorf S., Rose M.G., Abhari R.S., Modeling of film cooling—Part I: experimental study of flow structure
[8]  
McGovern K., Leylek J., A detailed analysis of film cooling physics: part II—Compound-angle injection with cylindrical holes, J. Turbomach., 122, 1, pp. 113-121, (2000)
[9]  
Mazaheri K., Kiani K.C., Karimi M., Application of a modified algebraic heat-flux model and second-moment-closure to high blowing-ratio film-cooling and corrugated heat-exchanger simulations, Appl. Therm. Eng., 124, pp. 948-966, (2017)
[10]  
Sinha A., Bogard D., Crawford M., Film-Cooling Effectiveness Downstream of a Single Row of Holes with Variable Density Ratio, (1991)