Abstract
Film cooling is a process that is used to protect turbine vanes in a gas turbine engine from exposure to hot combustion gases. In this paper, we have conducted the time-dependent analysis of film cooling by the large-eddy-simulation (LES) model. We have obtained static-temperature contours, pressure contours, velocity vectors and temperature plot at y = 12.7 mm iso-surface at different time intervals such as 10, 20.37 and 40.74 s. Significant results have been obtained.
Acknowledgements
The authors are highly indebted to the Fluid Particle Research Laboratory at the Indian Institute of Technology Roorkee, Roorkee 247667, Uttaranchal, India, for providing the FLUENT 6.2 software package for this analysis.