Effect of coolant temperature and mass flow on film cooling of turbine blades

Thin-layer approximation and algebraic model for separated turbulentflows

Betty Baldwin, Harvard Lomax · 16th Aerospace Sciences Meeting · 1978 · 3.3K citations

Engineering, Aerospace Engineering, Aerodynamics +16

Discrete-Jet Film Cooling: A Comparison of Computational Results With Experiments

James H. Leylek, R. D. Zerkle · Journal of Turbomachinery · 1994 · 271 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade

Riccardo Graziani, M. F. Blair, J. R. Taylor et al. · Journal of Engineering for Power · 1980 · 196 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Calculation of a circular jet in crossflow with a multiple-time-scale turbulence model

S.-W. Kim, Thomas J. Benson · International Journal of Heat and Mass Transfer · 1992 · 80 citations · Full text

Engineering, Aerospace Engineering, Physics +14

Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades

Vijay K. Garg, Raymond E. Gaugler · Journal of Turbomachinery · 1997 · 65 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +17