The last 50 years has witnessed significant improvement in film cooling technologies while
transpiration cooling is still not implemented in turbine airfoil cooling. Although transpiration …

The last 50 years has witnessed significant improvement in film cooling technologies while
transpiration cooling is still not implemented in turbine airfoil cooling. Although transpiration …

Transpiration cooling has always been the dream of gas turbine high temperature
component design. The uniform coolant coverage and enhanced heat transfer in porous …

Transpiration cooling is an effective method to protect high heat flux surfaces such as rocket
combustion chambers. However, this technology is currently not applicable for turbine …

Film cooling and thermal barrier coating are the most common external cooling techniques
used for gas turbine components. In film cooling, coolant air is brought to the external …

This article attempts to provide a cooling performance comparison of various mass transfer
cooling methods and different cooling media through two experiments. In the first …

Laser additive manufacturing (LAM) is an emerging technology capable of fabricating
complex geometries not possibly made by investment casting methods for gas turbine …

Transpiration cooling is able to provide more uniform coolant coverage than film cooling to
effectively protect the component surface from contacting the hot gas. Due to numerous …

Transpiration Cooling is an effective cooling technology to protect hot section components
such as gas turbine airfoils, rocket heads and space craft. This external cooling method has …

The present study experimentally evaluates the adiabatic film cooling effectiveness of a
gaseous transpiration cooling concept based on a family of nature-inspired triply periodic …