Designing film cooling for the leading-edge area of a turbine vane is much challenging due
to the highest thermal load, flow stagnation, as well as distorted incoming flows …

Deposition studies were conducted using two impingement jet facilities: a 60 m/s cold jet
(830–950 K) impinging on a heated Hastelloy-X surface (1033–1255 K) and a 215 m/s hot …

The presence and accretion of airborne particulates, including ash, sand, dust, and other
compounds, in gas turbine engines can adversely affect performance and life of …

In jet engines and gas turbines, the deposition phenomenon is attributed to the adhesion of
molten droplets on walls. In this study, numerical simulations of the deposition phenomena …

Film cooling from fan-shaped holes is an essential cooling technology in modern gas
turbines. The cooling performance degradation and life reduction of high-temperature …

In this paper, we analyze the impact of in-service deterioration on the overall thermal
performance (metal effectiveness) of heavily cooled high-pressure nozzle guide vanes of a …

In order to have a further insight into the dynamic build-up process of particle deposits within
the high-pressure turbine stator of an aeroengine and also into their effects on aerodynamic …

Characteristics of particle migration and deposition were numerically investigated in
presence of aggressive swirl at the turbine inlet. The isolated effects of the inlet swirl were …

This paper presents a review of particle deposition research in film-cooled gas turbines
based on the recent open literature. Factors affecting deposition capture efficiency and film …

Ash particle deposition in a high-pressure turbine stage was numerically investigated using
steady Reynolds-averaged Navier-Stokes (RANS) and unsteady Reynolds-averaged Navie …