Thermoacoustic oscillations associated with transverse acoustic modes are routinely
encountered in combustion chambers. While a large literature on this topic exists for rockets …

Combustion instability remains a critical issue limiting the development of low-emission,
lean-premixed (LPM) gas turbine combustion systems. The present work provides a …

Recent developments in numerical schemes, turbulent combustion models and the regular
increase of computing power allow Large Eddy Simulation (LES) to be applied to real …

This paper investigates one issue related to Large Eddy Simulation (LES) of self-excited
combustion instabilities in gas-fueled swirled burners: the effects of incomplete mixing …

The interaction of a helical precessing vortex core (PVC) with turbulent swirl flames in a gas
turbine model combustor is studied experimentally. The combustor is operated with air and …

COMBUSTION oscillations are frequently encountered during the development of many
combustion chambers for gas turbines [1–4]. To date, these oscillations cannot be predicted …

While most academic set ups used to study combustion instabilities are limited to single
burners and are submitted mainly to longitudinal acoustic modes, real gas turbines exhibit …

Large-Eddy Simulation (LES) has been used to analyze the occurrence and the causes of
cycle-to-cycle combustion variations in a spark ignited four-valve single cylinder engine …

Recent investigations into the rotating detonation phenomenon have involved its inception
and sustenance in hollow combustors, in contrast to the traditional annular rotating …

Although Large Eddy Simulations (LES) have demonstrated their potential in simple
academic combustion chambers, their application to real gas turbine chambers requires …