An overview of the science and technology involved in today's turbine engines is presented
with specific focus on the critical rotational-to-stationary interfaces comprising axial turbine …

Calculations were performed to simulate the tip flow and heat transfer on the GE-E3 first-
stage turbine, which represents a modern gas turbine blade geometry. Cases considered …

The primary focus of this paper is convective heat transfer in axial flow turbines. Research
activity involving heat transfer generally separates into two related areas: predictions and …

Heat transfer coefficient and static pressure distributions are experimentally investigated on
a gas turbine blade tip in a five-bladed stationary linear cascade. The blade is a two …

A combined experimental and computational study has been performed to investigate the
detailed distribution of convective heat transfer coefficients on the first-stage blade tip …

Experimental investigations are performed to measure the detailed heat transfer coefficient
and static pressure distributions on the squealer tip of a gas turbine blade in a five-bladed …

The flow through the tip clearance region of a transonic compressor rotor (NASA rotor 37)
was computed and compared to aerodynamic probe and laser anemometer data. Tip …

A combined experimental and computational study has been performed to investigate the
detailed distribution of convective heat transfer coefficients on the first-stage blade tip …

Detailed heat transfer coefficient distributions on a gas turbine squealer tip blade were
measured using a hue detection based transient liquid-crystals technique. The heat transfer …

Detailed heat transfer coefficient distributions on a squealer tip of a gas turbine blade were
measured using a hue detection based transient liquid crystals technique. The heat transfer …