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 …

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 …

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 …

A great number of studies have been conducted on a film cooling for turbine blades, which is
to prevent thermal damage on blades originated from high turbine inlet temperature …

Gas turbine components subjected to high temperatures can benefit from improved designs
enabled by metal additive manufacturing (AM) with nickel alloys. Previous studies have …

Transpiration cooling using liquid coolants is considered one of the most promising thermal
protection techniques for new generation aerospace vehicles. The leading edges are …

The limits of gas turbine technology are heavily influenced by materials and manufacturing
capabilities. Lately, incremental performance gains responsible for increasing the allowable …

The overall cooling effectiveness of a plane 152 mm square transpiration wall was
measured on a simulated gas turbine combustion chamber. Boundary layer temperature …

Additive manufacturing (AM) provides the ability to fabricate highly customized internal
cooling passages that are relevant to gas turbine components. This experimental study …

Gas turbine blade trailing edge cooling is challenging because of the stringent geometrical
constraints driven by aerodynamics and thermal stresses. The blade topology becomes …