The intrinsic thermoacoustic (ITA) feedbackloop constitutes a coupling between flow, flame and acoustics that does not involve the natural acoustic modes of the system. One recent study showed that ITA modes in annular combustors come in significant number and with the peculiar behavior of clusters, i.e. several modes with close frequencies. In the present work an analytical model of a typical annular combustor is derived via Riemann invariants and Bloch theory. The resulting formulation describes the full annular system as a longitudinal combustor with an outlet reflection coefficient that depends on frequency and the azimuthal mode order. The model explains the underlying mechanism of the clustering phenomena and the structure of the clus...
The subject of this dissertation are thermoacoustic instabilities in combustion chambers with discre...
We present a unified, physics-based low-order modeling approach to can-annular combustors, combining...
Heavy-duty gas turbines are commonly designed with can-annular combustors, in which all flames are p...
The intrinsic thermoacoustic (ITA) feedbackloop constitutes a coupling between flow, flame and acous...
Thermoacoustic systems can exhibit self-excited instabilities of two nature, namely cavity modes or ...
Rotationally symmetric annular combustors are of practical importance because they generically resem...
We propose a general classification of all the modes of a given thermoacoustic system into two sets:...
In annular combustion systems, thermoacoustic eigenmodes can manifest as standing waves, traveling w...
Thermoacoustic instabilities in annular gas turbine combustors often involve modes which vary in bot...
The adoption of lean premixed prevaporised combustion systems can reduce NOx emissions from gas turb...
International audienceLongitudinal low-frequency thermoacoustic unstable modes in combustion chamber...
In annular combustion systems, azimuthal thermoacoustic modes manifest themselves predominantly as t...
International audienceNonlinear coupling between azimuthal and axisymmetric modes in annular combust...
This paper first characterizes the acoustic field of two annular combustors by means of data from ac...
Annular combustion chambers of gas turbines and aircraft engines are subject to unstable azimuthal t...
The subject of this dissertation are thermoacoustic instabilities in combustion chambers with discre...
We present a unified, physics-based low-order modeling approach to can-annular combustors, combining...
Heavy-duty gas turbines are commonly designed with can-annular combustors, in which all flames are p...
The intrinsic thermoacoustic (ITA) feedbackloop constitutes a coupling between flow, flame and acous...
Thermoacoustic systems can exhibit self-excited instabilities of two nature, namely cavity modes or ...
Rotationally symmetric annular combustors are of practical importance because they generically resem...
We propose a general classification of all the modes of a given thermoacoustic system into two sets:...
In annular combustion systems, thermoacoustic eigenmodes can manifest as standing waves, traveling w...
Thermoacoustic instabilities in annular gas turbine combustors often involve modes which vary in bot...
The adoption of lean premixed prevaporised combustion systems can reduce NOx emissions from gas turb...
International audienceLongitudinal low-frequency thermoacoustic unstable modes in combustion chamber...
In annular combustion systems, azimuthal thermoacoustic modes manifest themselves predominantly as t...
International audienceNonlinear coupling between azimuthal and axisymmetric modes in annular combust...
This paper first characterizes the acoustic field of two annular combustors by means of data from ac...
Annular combustion chambers of gas turbines and aircraft engines are subject to unstable azimuthal t...
The subject of this dissertation are thermoacoustic instabilities in combustion chambers with discre...
We present a unified, physics-based low-order modeling approach to can-annular combustors, combining...
Heavy-duty gas turbines are commonly designed with can-annular combustors, in which all flames are p...