The effect of rail crown film hole injection angle and blowing ratio on the flow and cooling performance of the squealer tip in a turbine blade

Axial Turbine Blade Tips: Function, Design, and Durability

Ronald S. Bunker · Journal of Propulsion and Power · 2006 · 270 citations

Engineering, Aerospace Engineering, Mechanical Engineering +13

Rotor-Tip Leakage: Part I—Basic Methodology

T. C. Booth, P. R. Dodge, H. Kent Hepworth · Journal of Engineering for Power · 1982 · 172 citations

Engineering, Aerospace Engineering, Computational Fluid Dynamics +12

The Effect of Blade Tip Geometry on the Tip Leakage Flow in Axial Turbine Cascades

F. J. G. Heyes · Journal of Turbomachinery · 1992 · 150 citations

Engineering, Aerospace Engineering, Aerodynamics +12

Heat Transfer Coefficients on the Squealer Tip and Near-Tip Regions of a Gas Turbine Blade With Single or Double Squealer

Jae Su Kwak, Jaeyong Ahn, Je-Chin Han et al. · Journal of Turbomachinery · 2003 · 125 citations

Engineering, Mechanical Engineering, Aerodynamics +15

Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer

Gm. S. Azad, Je-Chin Han, Ronald S. Bunker et al. · Journal of Heat Transfer · 2002 · 111 citations

Engineering, Aerospace Engineering, Aerodynamics +12