The combustion chamber is the most critical part of a gas turbine. The chamber had to be
designed so that the combustion process to sustain itself in a continuous manner and the …

Combustion noise in gas turbine engines has recently become a relevant source of noise in
the aircraft due to the appearance of new burner architectures that are intrinsically more …

Temperature uniformity after a mixing process plays a very important role in many
applications. Non-uniform temperature at the entrance of the turbine in gas turbine systems …

This paper presents the effects of various inlet geometries on swirling flow and a study of the
flow behavior of air in the can combustor using a CFD model. In this work, the standard k-ɛ …

three dimensional numerical investigation of the combustion of methane air mixture in gas
turbine Can-combustor by using CFD with CFX solver is presented in this study. The …

In this study, two-blade and four-blade swirl inserts with 180°, 270° and 360° pitch angles, φ
each were used for the first time to generate swirling flow in plunging water jets to enhance …

This paper presents a study on a novel axial flow swirler concept for gas turbine engines,
which plays a crucial role in achieving desired air motion patterns with swirl. The main …

The main purpose of this paper is to study the internal flow effect of varying the swirl number
inside the combustor. The flow field inside the combustor is controlled by the liner shape and …

Numerical analysis of computational fluid dynamics (CFD) is one of technologies that can be
minimized the experimental cost. This paper is presents the isothermal swirling turbulent …

This paper presents the computational analysis of the dilution process involved in gas
turbines order to cool the combustion gases to the desired temperature before it enters the …