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/effusion cooling systems have been studied extensively over the past few
decades to constantly improve cooling performance as the turbine inlet temperature of …

A novel double-wall cooling configuration with im**ement induced swirling film cooling is
investigated in present paper. The effects of im**ement inclined angle, blowing ratio, film …

In this work, time-resolved quantitative light sheet technique is used to capture the transient
outflow performances of the laminated cooling in turbine vane leading edges. A series of …

The double-wall cooling as one of the most important cooling techniques of the hot-end
components of aero-engine, the heat transfer performance of double-wall cooling structure …

This paper presents a flow and heat transfer investigation on multi-row dimpled film cooling
in the double-wall configuration, considering important flow and geometrical characteristics …

The effects of micro-pin characteristics on flow and heat transfer of a circular im**ing jet
are studied both experimentally and numerically. The studies are carried out for a single jet …

For a further improvement of im**ement jet array heat transfer in a corrugated channel, a
wing-shaped structure design is proposed to weaken crossflow degradation. The …

The present study is to investigate the effect of gap height on heat/mass transfer for
im**ement/effusion cooling of gas turbine hot components, using a hollow cylinder …

Experimental investigations of mainstream turbulence intensity (Tu) effect on conjugate heat
transfer performances, total pressure loss and solid thermal deformations of vane laminated …