The present review covers the heat transfer literature published in 2004 in English
language, including some translations of foreign language papers. Though extensive, some …

Adiabatic effectiveness (η) is the most important parameter for evaluating film cooling
capacity. For turbine blades, it is usually based on the scaling criteria to achieve the …

Inadequate design of film cooling holes can significantly reduce film cooling effectiveness of
turbine blades, compromising high temperature resistance. By comparing experimental …

In this study, the film cooling performance of a three-dimensional (3D) hybrid slot–effusion
configuration and its advantages over a baseline pure 3D slot cooling are investigated in …

This paper investigates effects of geometrical and coolant flow parameters for a three-row
compound angle hole design over a flat plate. These included β=+ 45° and− 45°, in-line and …

In the suction surface gill region of the turbine blade, three representative regions with a
favorable pressure gradient (FPG), adverse pressure gradient (APG), and pressure gradient …

The mechanism of transpiration cooling with liquid phase change is numerically investigated
to protect the thermal structure exposed to extremely high heat flux. According to the results …

During the operation of turbomachinery, there are sometimes sudden changes in some flow
parameters, which in turn affect the cooling characteristics on the blade. It is also necessary …

An inclined turbulent jet discharging a passive scalar into a turbulent crossflow is
investigated under conditions of favorable, zero and adverse streamwise pressure gradient …

In the present research, the influence of the particle dispersion onto the continuous phase in
film cooling application was analysed by means of numerical simulations. The interaction …