Large-Eddy Simulation of double-row compound-angle film cooling: Setup and validation
Film cooling is an important technique allowing to increase the thermal efficiency of gas turbines. By blowing cool air through an array of small holes in the turbine blades a thin fluid film is set up shielding the blades from the hot gas arriving from the combustion chamber. This work presents a Large-Eddy Simulation of a particular film-cooling configuration known to provide a high level of effectiveness. It incorporates spanwise rows of holes which, by pairwise combination, generate a so-called anti-kidney-vortex. The simulation setup employs the Navier-Stokes code NSMB for compressible flow including the Approximate Deconvolution Model for subgrid turbulence modeling, the Synthetic-Eddy Method for turbulent inflow generation and reflection-reducing outflow boundary conditions. The setup is first validated by simulations of standard flat-plate turbulent boundary-layer flow without blowing. Results of the film-cooling simulation are then compared with related experimental data. They show reasonable agreement of the cooling effectiveness and temperature distribution, thus confirming the validity of the simulation approach which will be used in future studies of film cooling. (C) 2010 Elsevier Ltd. All rights reserved.
large-eddy simulation film cooling approximate deconvolution model synthetic-eddy method turbulent boundary-layer jet in crossflow compound angle double row kidney-vortex anti-kidney-vortex les adm