Numerical approach to film cooling effectiveness over a plate surface with coolant impingement

Camci, C, Arts, T. Experimental Heat Transfer Investigation Around the Film-Cooled Leading Edge of a High-Pressure Gas Turbine Rotor Blade. ASME Journal of Engineering for Gas Turbines and Power, 1985, 107: 1016–1021

Walker, L A, Markland, E. Heat Transfer to Turbine Blading in the Presence of Secondary Flow. International Journal of Heat and Mass Transfer, 1965, 8: 729–748

Walters, D K, Leylek, J H. A Detailed Analysis of Film-Cooling Physics: Part I-Streamwise Injection with Cylindrical Holes. ASME Journal of Turbomachinery, 2000, 122: 102–112

McGovern, K T, Leylek, J H. A Detailed Analysis of Film Cooling Physics: Part II-Compound-Angle Injection with Cylindrical Holes. ASME Journal of Turbomachinery, 2000, 122: 113–121

Hyams, D G, Leylek, J H. A Detailed Analysis of Film Cooling Physics: Part III-Streamwise Injection With Shaped Holes. ASME Journal of Turbomachinery, 2000, 122: 122–132

Brittingham, R A, Leylek, J H. A Detailed Analysis of Film Cooling Physics: Part IV-Compound-Angle Injection with Shaped Holes. ASME Journal of Turbomachinery, 2000, 122: 133–145

Garg, V K. Heat Transfer Research on Gas Turbine Airfoils at NASA GRC. International Journal of Heat and Fluid Flow, 2002, 23: 109–136

Launder, B E, Sharma, B I. Application of the Energy Dissipation Model of Turbulence to the Calculation of Flow Near a Spinning Disc. Letter in Heat and Mass Transfer, 1974, 1(2): 131–138