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 characteristics for flat and squealer turbine tip geometries are studied in
the von Karman Institute Isentropic Light Piston Compression Tube facility, CT-2, at different …

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 …

The presence of turbine blade tip clearance can cause tip leakage losses and enhance the
thermal load on the tip region. The continuously increasing inlet temperature of the turbine …

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 …

In axial turbine, the tip clearance flow occurring in rotor blade rows is responsible for about
one-third of the aerodynamic losses in the blade row and in many cases is the limiting factor …

Heat transfer continues to be a major field of interest to engineering and scientific
researchers, as well as designers, developers, and manufacturers. Considerable effort has …

This study investigates the effect of a squealer tip geometry arrangement on heat transfer
coefficient and static pressure distributions on a gas turbine blade tip in a five-bladed …

This paper deals with an experimental investigation of aerodynamic characteristics of full
and partial-length squealer rims in a turbine stage. Full and partial-length squealer rims are …