Effects of transverse divider wall within the squealer cavity on the performance of a novel squealer tip with rail crown holes for the gas 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

Heat Transfer and Pressure Distributions on a Gas Turbine Blade Tip

Gm. S. Azad, Je-Chin Han, Shuye Teng et al. · Journal of Turbomachinery · 2000 · 166 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Energy Efficient Engine high pressure turbine component test performance report

L. P. Timko · NASA STI Repository (National Aeronautics and Space Administration) · 1984 · 160 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +17

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

Turbine Blade Tip Heat Transfer in Low Speed and High Speed Flows

Andrew P. S. Wheeler, Nicholas R. Atkins, L. He · Journal of Turbomachinery · 2011 · 121 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17