Results The reported tests were performed at a nominally unstable condition, with an
instability frequency of 461 Hz. The forcing frequencies investigated ranged from 150 to 430 …

This paper describes an experimental investigation of the nonlinear interactions between
self-excited and driven oscillations in a premixed swirl-stabilized combustor. This interaction …

Instability modes were investigated and controlled in an experimental low-emission swirl
stabilised combustor, in which the acoustic boundary conditions were modified to increase …

Combustion instabilities in lean premixed combustors are often manifested by pressure
oscillations that can result in serious performance degradation and even cause failure …

Two different types of combustion instabilities were excited in a scale model partially
premixed swirl burner/furnace by modifying the downstream boundary conditions. Both …

In this study, experimental measurements are performed on a swirl-stabilized combustor to
study the nonlinear combustor dynamic characteristics under acoustic excitations. The …

Measurements of self-excited combustion instability were performed in a lean-premixed,
swirl-stabilized, gas turbine combustor in order to characterize the interaction between the …

The present work deals with active control of combustion instabilities in a swirlstabilized
spray combustor. The combustor was characterized by a thermo-acoustic instability at …

Interaction between flow instabilities and acoustic resonant modes and their effect on heat
release were investigated and controlled in an experimental low-emission swirl stabilized …

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 …