A systematic compilation and evaluation of turbulent spray flame combustion data acquired
from lab-scale spray-burners and CFD models validated with these are presented. Previous …

This study investigates H 2-air flames obtained with a laboratory scale coaxial dual-swirl
injector in which fuel and oxidizer are injected separately. Two flame archetypes are …

Large eddy simulations (LES) of self-excited spray combustion instability in an aero-engine
combustor are performed to investigate the mechanisms of combustion instability. Three …

Computational prediction of thermoacoustic instabilities arising in gas turbine and aero-
engine combustors still remains a challenge especially if fuel is injected in a liquid spray …

Identifying combustion regimes in terms of premixed and non-premixed characteristics is an
important task for understanding combustion phenomena and the structure of flames. A …

A detailed study of ignition mechanisms in aeronautical burners is presented. Even in global
lean conditions, liquid fuel injection leads to a strong stratification of the mixture and the …

This study deals with the fundamental problem of combustion dynamics in gas turbine
combustors operating with liquid fuel. In this framework the present work proposes the study …

The high-temperature zone of a laboratory staged swirl gas turbine combustor was studied
under different Stratification Ratios (SR) based on experimentally validated Large Eddy …

In order to reduce global warming, new energy fuels that use waste biomass to replace
traditional coal are rapidly developing. The main purpose of this study is to investigate the …

Lean premixed prevaporized combustors with a centrally staged scheme are capable to
reduce NOx emissions. Ignition is one of the key performances of the centrally staged …