Turbine inlet temperature has continuously increased to improve gas turbine performance
during the past few decades. Although internal convection cooling and traditional film …

Im**ement and film cooling techniques are emerging areas in the turbine component
cooling technology. Vast amount of information on this subject is available in the literature …

To address the complex structures, large out-of-tolerance issues, and inconsistent quality of
double-walled turbine blades, a map** relationship between the structure and …

Double-wall effusion cooling system is a promising cooling solution for next-generation gas
turbines. Thinning the blade wall can bring the coolant closer to the hot stream, thereby …

The ambition for increasing gas turbine efficiency beyond current levels through the
elevation of gas temperatures demands substantial progress in turbine blade cooling …

Im**ement/effusion cooling is regarded as a highly efficient cooling structure and has
been widely adopted in various energy-dependent scenarios. It often exhibits crossflow …

Transpiration cooling is a promising cooling measure for high-temperature components in
gas turbines. Although the flow and heat transfer characteristics of transpiration cooling have …

In this paper, the overall cooling effectiveness of double wall cooling structures with pins is
experimentally investigated on the low-speed wind tunnel. The analysis of the single cooling …

Laminated cooling coupled by surface thermal barrier coating (TBC) has a large potential to
provide the effective protection to components in next-generation gas turbines. However, the …

Im**ement cooling is an important turbine blades cooling technique, but it is often not as
efficient as required due to the deflection of downstream jets caused by crossflow. In this …