This paper demonstrates cross-frequency coupling between pressure, heat release rate, fuel
spray and velocity oscillations in a model aeronautical gas turbine combustor operating at a …

Dynamics of thermoacoustics oscillations occurring in a liquid fueled aeronautical gas
turbine model combustor burning Jet A fuel were investigated experimentally at a pressure …

This document presents an investigation of the self-excited coupling mechanisms that occur
to produce both low-amplitude intermittent, as well as high-amplitude limit-cycle pressure …

This paper analyzes intermittent self-excited thermoacoustic oscillations in which the
pressure (P′) and heat release rate (q̇′) fluctuations are harmonically coupled. That is to …

A framework is presented for analyzing the local instantaneous phase difference between
non-stationary heat release rate and pressure oscillations that is appropriate for use in high …

Thermoacoustic combustion oscillation and vibration experienced in a gas turbine at
operation is reported. The oscillation manifested itself at two distinct frequencies …

This paper describes an experimental investigation of the response of the flame in a lean,
premixed combustor to imposed acoustic oscillations. The ultimate objective of this work is to …

A gas turbine model combustor for partially premixed swirl flames was equipped with an
optical combustion chamber and operated with CH 4 and air at atmospheric pressure. The …

The prediction of high-frequency acoustic oscillations in gas turbine combustors is an
important issue, related to engine performance, NOx emissions, component lifetime and …

This paper presents the experimental investigation of pulsation-amplitude-dependent flame
dynamics associated with transverse thermoacoustic oscillations at screech level …