1. AI-Zurfi, N. and Turan, A., LES of rotational effects on film cooling effectiveness and heat transfer coefficient in a gas turbine blade with one row of air film injection, International Journal of Thermal Sciences, Vol.99 (2016), pp.96-112.
2. Bogard, D. G. and Thole, K. A., Gas Turbine Film Cooling, AIAA Journal of Propulsion and Power, Vol.22, No.2 (2006), pp.249-270.
3. Bunker, R. S., A review of shaped hole turbine film-cooling technology, ASME Journal of heat transfer, Vol.127, No.4 (2005), pp.441-453.
4. Dees, J. E., Bogard, D. G., Ledezma, G. A., Laskowski, G. M. and Tolpadi, A. K., Experimental measurements and computational predictions for an internally cooled simulated turbine vane, ASME Journal of Turbomachinery, Vol.134 (2012), pp.061003-1-9.
5. Drost, U. and Bölcs, A., Investigation of detailed film cooling effectiveness and heat transfer distributions on a gas turbine airfoil, ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition, Paper No.98-GT-020.