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

The main objective of this work was to investigate the beating behavior of acoustically self-
excited instabilities in dual swirl combustors. This was achieved by measuring fluctuations in …

The aim of this present study is to examine the critical role of air-fuel equivalence ratio Ф and
air flow rate on triggering self-excited thermoacoustic oscillations in a swirling combustor …

The combustion instability of a partially premixed swirl burner is investigated by
experimental tests and numerical modeling. The experimental results show that the …

The coupled behavior of the acoustic pressure and the heat release rate fluctuations is
studied in a swirl-stabilized combustor during the transition of system dynamics from …

Industrial combustion systems such as power generation gas turbines, rocket motors,
furnaces and boilers often face the problem of large-amplitude self-excited pressure …

Combustion instability is a common thermoacoustic coupling problem in combustion
systems, and the pressure oscillations generated inevitably damage the combustion system …

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 …

In the start-up process of practical gas turbine applications, the modulation of operating
condition, especially the variation of global equivalence ratios (ϕ glo), could cause the …

In the present work, the combustion instability of a premixed swirl combustor was
experimentally and theoretically investigated. Results show that both intrinsic …