Gas turbines are widely used for aircraft propulsion, land-base power generation, and other
industrial applications like trains, marines, automobiles, etc. To satisfy the fast development …

The tip-leakage flow in a turbomachinery cascade is studied using large-eddy simulation
with particular emphasis on understanding the underlying mechanisms for viscous losses in …

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 …

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 …

Abstract The requirements of Liquid Propellant Rocket Engine (LPRE) are high for thrust,
specific impulse, and flow rate; thus, its components also have strict requirements. For the …

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 …

Experimental investigations were performed to measure the detailed heat transfer
coefficients and film cooling effectiveness on the squealer tip of a gas turbine blade in a five …