Hydrogen can represent an option for a low emission gas turbine if low NOx combustion
systems are developed. This paper describes the design and the investigations carried out …

Unsteady component interaction represents a crucial topic in turbomachinery design and
analysis. Combustor/turbine interaction is one of the most widely studied topics both using …

Cooling performance is experimentally and numerically investigated in an effusion-cooled,
swirl-stabilized three-sector gas turbine combustor at realistic reacting flows. The …

Effusion cooling is often regarded as one of the critical techniques to protect solid surfaces
from exposure to extremely hot environments, such as inside a combustion chamber where …

Fuel injection and distribution play an important role in the formation and migration of hot
streaks in gas turbine combustors and determine the exit temperature uniformity especially …

In many industrial applications, the mechanical integrity of a surface operating under large
thermal loads is ensured by injecting a cold fluid through a series of hole along the surface …

Conjugate heat transfer characteristics of the effusion cooling applied on the swirl-stabilized
combustor liner is experimentally and numerically investigated in a three-nozzle gas turbine …

The design of modern gas turbines cooling systems cannot be separated from the use of
computational fluid dynamics (CFD) and the accurate estimation of the effect of film cooling …

Abstract Full-scale Computational Fluid Dynamics (CFD) numerical simulations can
accurately predict the heat flux and metal wall temperature of gas turbine combustor liners …

Detailed effusion cooling feature on both inner and outer liner of a scaled annular combustor
equipped with three axial swirlers has been investigated experimentally under both non …