T Poinsot - Proceedings of the Combustion Institute, 2017 - Elsevier
This paper presents recent progress in the field of thermoacoustic combustion instabilities in propulsion engines such as rockets or gas turbines. Combustion instabilities have been …
Accurate prediction of limit cycle oscillations resulting from combustion instability has been a long-standing challenge. The present work uses a coupled approach to predict the limit …
A coupled numerical approach is investigated for predicting combustion instability limit cycle characteristics when the combustor contains a long flame. The test case is the ORACLES …
A combustion instability in a combustor terminated by a nozzle is analysed and modelled based on a low-order Helmholtz solver. A large eddy simulation (LES) of the corresponding …
Progress in analytical methods to predict and control azimuthal combustion instability modes in annular chambers | Physics of Fluids | AIP Publishing Skip to Main Content …
L Li, D Zhao - Aerospace Science and Technology, 2015 - Elsevier
Many aero-engine and gas turbine combustion systems are in choked configuration. These combustors are more prone to thermoacoustic instability. Thus there is a need to …
GA Mensah, G Campa… - … of Engineering for …, 2016 - asmedigitalcollection.asme.org
Most annular combustors feature a discrete rotational symmetry so that the full configuration can be obtained by copying one burner-flame segment a certain number of times around the …
Thermoacoustic instability occurs in many practical combustion systems. These systems are non-normal and associated with transient growth of acoustic disturbances. If the transient …
M Meindl, CF Silva, W Polifke - Combustion and Flame, 2021 - Elsevier
This work demonstrates that a hybrid approach for linear thermoacoustic stability analysis that combines the Linearized Navier–Stokes Equations (LNSE) with a global Flame Transfer …