Large-Eddy Simulations of a Cylindrical Film Cooling Hole

被引:16
作者
Johnson, Perry L. [1 ]
Kapat, Jayanta S. [1 ]
机构
[1] Univ Cent Florida, Ctr Adv Turbine & Energy Res, Lab Turbine Aerodynam Heat Transfer & Durabil, Dept Mech Mat & Aerosp Engn, Orlando, FL 32816 USA
关键词
DETAILED ANALYSIS; BOUNDARY-LAYER; STREAMWISE INJECTION; PHYSICS; FLOW; GENERATION; DOWNSTREAM;
D O I
10.2514/1.T3890
中图分类号
O414.1 [热力学];
学科分类号
摘要
Large-eddy simulations are used to explore the unsteady jet-in-crossflow interactions arising from discrete hole film cooling from a cylindrical hole. The numerical grids are created using GridPro and solved in OpenFOAM. A recycling-rescaling technique is used to generate a realistic turbulent incoming boundary layer upstream of injection. The simulations match the conditions of an experiment in the open literature for the robust validation of the numerical solution and turbulence modeling. The current study tests the ability of large-eddy simulations in predicting film cooling flows using detailed experimental measurements. The large-eddy simulation results compared favorably with the experimental data except in areas close to the injection site and close to the wall. Grid resolution is discussed in terms of the percent turbulent kinetic energy resolved and related to the success of the large eddy simulation predictions in different regions of the jet. No substantial benefit was seen by using a dynamic Smagorinsky model for the subgrid turbulent heat fluxes instead of a constant subgrid Prandtl number. The trajectories, spreading rates, and large turbulent structures of the jet are discussed in terms of the hydrodynamic parameters such as velocity ratio and momentum ratio.
引用
收藏
页码:255 / 273
页数:19
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