Interference mechanisms of acoustic/convective disturbances were experimentally
investigated in a swirl-stabilized lean-premixed gas turbine combustor operated with natural …

Constructive interference between heat release rate and acoustic perturbation is
responsible for the growth of acoustic pressure amplitudes, leading to high-amplitude …

The effect of inlet swirl on the flow development and combustion dynamics in a lean-
premixed swirl-stabilized combustor has been numerically investigated using a large-eddy …

A comprehensive study on influences of hydrodynamic features of a swirling flow on
thermoacoustic instabilities in a swirl stabilized combustor is performed by using large eddy …

This article describes an experimental investigation of the forced response of a swirl-
stabilized partially premixed flame when it is subjected to acoustic velocity and equivalence …

In this experimental study, the combined effect of spatial and temporal variations of fuel–air
mixture on self-excited combustion instabilities in a gas-turbine model combustor (∼ 60 kW) …

Modern gas turbines use lean premixed combustion to achieve the best compromise
between pollutant emissions and efficiency. This type of combustion increases the flame …

This paper describes an analysis of the unsteady flow field in swirl flames subjected to
transverse acoustic waves. This work is motivated by transverse instabilities in annular gas …

The impact of premixer swirl number, S, and overall fuel equivalence ratio, Φ, on the stability
of a model swirl-stabilized, lean-premixed gas turbine combustor has been numerically …

Lean premixed combustors are highly susceptible to combustion instabilities, caused by the
coupling between heat release fluctuations and combustor acoustics. In order to predict the …