Transpiration cooling is expected to be one of the most effective cooling technologies for gas
turbine blades. However, dust deposition can easily lead to pore plugging, which limits its …

Transpiration cooling is an effective method of protecting high-temperature components.
However, this technology is currently not applicable to turbine blades because conventional …

Transpiration cooling is one of the most efficient cooling technologies to protect hot section
components such as turbine airfoils, missile heads and shells of rockets or space craft. This …

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 …

Comprehensive experimental and numerical studies were performed to determine cooling
film effectiveness of transpiration cooling over porous materials. The cooling film …

The reasonable distribution of coolant heat sink is an effective way to solve thermal ablation
and improve the thermal protection effect of transpiration cooling. Intermittent transpiration …

Transpiration cooling based on a porous structure has an ultra-high cooling efficiency, which
is expected to be one solution to improve the cooling technology of aero-engine turbine …

As an active thermal protection technology with high cooling efficiency, transpiration cooling
can achieve effective thermal protection for turbine blades. However, most of the studies are …

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 …

This study aims to reveal the cooling benefits of the derived coolant film from partitioned
porous injectors for transpiration cooling. The near-wall flow development and the cooling …