Boundary-condition models of film-cooling holes for large-eddy simulation of turbine vanes

• Published in: International journal of heat and mass transfer Vol. 166; p. 120763
• Main Authors: Dupuy, D., Perrot, A., Odier, N., Gicquel, L.Y.M., Duchaine, F.
• Format: Journal Article
• Language: English
• Published: Oxford Elsevier Ltd 01.02.2021; Elsevier BV; Elsevier
• Subjects: Boundary conditions; Computational fluid dynamics; Cooling; Cooling systems; Cross flow; Engineering Sciences; Film cooling; Finite element method; Fluid flow; Fluid mechanics; Fluids mechanics; Industrial applications; Inhomogeneity; Large eddy simulation; Mechanics; Modelling; Nozzles; Physics; Solid surfaces; Thermal analysis; Thermics; Thin films; Turbines; Turbulence; Turbulent flow; Turbulent mixing; Vortices; Modelling; Large-eddy simulation; Film cooling
• ISSN: 0017-9310; 1879-2189
• DOI: 10.1016/j.ijheatmasstransfer.2020.120763

•An inhomogeneous turbulent boundary condition can model a cylindrical film-cooling hole.•The model also improves the predictions for laidback and fanshaped laidback holes.•The spatial inhomogeneity is particularly important for the near-hole behaviour of the flow.•Turbulence injection is crucial to immediately trigger the transition of the jet. In many industrial applications, the mechanical integrity of a surface operating under large thermal loads is ensured by injecting a cold fluid through a series of hole along the surface, forming a thin film of cool fluid shielding the solid surface from external heat. An accurate prediction of the heat transfer provided by these so-called film-cooling systems is crucial to ensure the durability of the cooled surfaces. However, the large-eddy simulation of film-cooling systems is complex and expensive because the in-hole flow must be meshed and simulated. To address this difficulty, the modelling of the film-cooling jet by mean of a dedicated boundary condition has recently been proposed. This paper investigates several potential improvements for this type of model in four geometries: an inclined cylindrical hole, a fanshaped hole and two fanshaped laidback holes. The analysis focuses on the comparison of a spatially uniform injection to a model taking into account velocity and temperature spatial variations at the hole exit. The study also compares a non-turbulent injection to a model with synthetic turbulence injection. The comparisons are first performed using a fine mesh to validate the approach, then using a coarse mesh representative of a mesh that could be used to simulate a cooled nozzle guide vane. The results show that both spatial inhomogeneity and turbulence injection significantly improve the cooling effectiveness predictions in a wide variety of cases. The spatial inhomogeneity is especially crucial for the near-hole behaviour of the flow while turbulence injection is particularly important when the destabilisation of the jet by the crossflow is not sufficient to immediately trigger transition. Using a very coarse mesh, the turbulent mixing is observed to be underestimated with all examined boundary-condition models and the behaviour of the jet is not correctly described for some of the configurations investigated. Although not sufficient, non-negligible improvements are nevertheless obtained with an inhomogeneous turbulent injection compared to the baseline uniform model.